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Thermosetting composites

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• Composite materials
• Thermosetting plastics

• Reinforced thermoset resin composites
• Thermoset composites

• An experimental feasibility study for the preparation of thermo-oxidatively stable Pyrrone laminates/ (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by H. R. Lubowitz, Langley Research Center, and TRW Systems Group (page images at HathiTrust)
• Effect of weight, density, and heat load on thermal shielding performance of phenolic nylon / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Andrew J. Chapman and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Engineering and the Advancement of Human Welfare: 10 Outstanding Achievements, 1964-1989, by National Academy of Engineering (page images with commentary at NAP)
• Thermal stresses induced in a composite model bridge structure : prepared for Missouri State Highway Dept. / (Rolla, Mo. : Civil Engineering Dept., University of Missouri-Rolla, 1977), by Jack H Emanuel, David John Wisch, United States. Federal Highway Administration, University of Missouri--Rolla. Civil Engineering Dept, and Missouri. State Highway Dept (page images at HathiTrust; US access only)
• Interface control and mechnanical property improvements in silicon carbide/titanium composites / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by William D. Brewer, Jalaiah Unnum, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Workshop on scaling effects in composite materials and structures / (Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1994), by Karen E. Jackson, San Diego University of California, Virginia Polytechnic Institute and State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Joining of advanced composites / ([Alexandria, Va. : Dept. of Defense], Dept. of the Army, Army Materiel Development and Readiness Command ; [Springfield, Va. : for sale by the National Technical Information Service], 1979), by United States. Army Materiel Development and Readiness Command, Andrew Devine, and Plastics Technical Evaluation Center (U.S.) (page images at HathiTrust)
• Two-year Wisconsin thermal loads for roof assemblies and wood, wood-plastic composite, and fiberglass shingles / (Madison, WI : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, [2005]), by Jerrold E. Winandy, Cherilyn A. Hatfield, Michael Grambsch, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Tensile strength of composite truss lumber as affected by veneer species and member width / (Asheville, N.C. : Southeastern Forest Experiment Station, 1984), by Robert H. McAlister and Building Technology United States. Division of Energy (page images at HathiTrust)
• Linear expansion design theory for COM-PLY panels / ([Asheville, N.C.] : U.S. Dept. of Agriculture, Forest Service, Southern Forest Experiment Station, 1981), by John W. Talbott, N.C.) Southeastern Forest Experiment Station (Asheville, Washington State University. Wood Technology Section, and Building Technology United States. Division of Energy (page images at HathiTrust)
• Local buckling of orthotropic truss-core sandwich / (Madison, Wis. : U.S. Forest Products Laboratory, 1973), by John J. Zahn and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Using wood composites as a tool for sustainable forestry : proceedings of scientific session 90, XXII IUFRO World Congress / (Madison, WI : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 2005), by Selim Salim Hiziroglu, Robert W Wellwood, Jerrold E. Winandy, Forest Products Laboratory (U.S.), and 22nd International Union of Forestry Research Organizations. IUFRO World Congress (page images at HathiTrust)
• Fundamentals of composite processing : proceedings of a workshop / (Madison, WI : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, [2004]), by Frederick A. Kamke, Jerrold E. Winandy, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Sonic fatigue design techniques for advanced composite aircraft structures : final report / (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, [1980]), by I. Holehouse and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Investigation of mechanical properties and metallurgical characteristics of a metallic chromium and magnesium oxide composite / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1963), by Charles R. Manning, Dick M. Royster, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Ralph L. Schacht, Richard J. Quentmeyer, Harold G. Price, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Composite materials for rail transit systems / (Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1988]), by Carl T. Herakovich, Zafer Gürdal, O. Hayden Griffin, United States. Urban Mass Transportation Administration, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Self-lubricating plasma-sprayed composites for sliding-contact bearings to 900 ̊C / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Harold E. Sliney and Lewis Research Center (page images at HathiTrust)
• Thermal loading in the laser holography nondestructive testing of a composite structure / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by H. K. Liu, Robert L. Kurtz, and George C. Marshall Space Flight Center. Space Sciences Laboratory (page images at HathiTrust)
• Eutectic superalloys strengthened by [delta], Ni₃Cb lamellae and [gamma]', Ni₃Al precipitates / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by F. D. Lemkey, Lewis Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Comparison of polyester, film-yarn composite, balloon materials subjected to shear and biaxial loading / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by R. J. Niccum, Langley Research Center, and G.T. Schjeldahl Company (page images at HathiTrust)
• Evaluation of energy absorption of new concepts of aircraft composite subfloor intersections / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Lisa E. Jones, Huey D. Carden, and Langley Research Center (page images at HathiTrust)
• Experimental evaluation of high-purity-silica reinforced ablative composites as nozzle sections of 7.8-inch-(19.8 CM) diameter throat storable-propellant rocket engine / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Donald A. Peterson and Lewis Research Center (page images at HathiTrust)
• Fatigue evaluation of composite-reinforced, integrally stiffened metal panels : summary / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by C. E. Dumesnil, Langley Research Center, and Vought Aeronautics Company (page images at HathiTrust)
• Development of lightweight aluminum compression panels reinforced by boron-epoxy infiltrated extrusions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Paul A. Roy, Jim Henshaw, John A. McElman, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Evaluation of cryogenic insulation materials and composites for use in nuclear radiation environments / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by R. E. Bullock, George C. Marshall Space Flight Center, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Boron/aluminum-graphite/resin advanced fiber composite hybrids / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by C. C. Chamis, Timothy L. Sullivan, Raymond F. Lark, and Lewis Research Center (page images at HathiTrust)
• Flight and ground tests of a very-low-density elastomeric ablative material / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by George C. Olsen, Andrew Chapman, and Langley Research Center (page images at HathiTrust)
• Holographic and ultrasonic detection of bond flaws in aluminum panels reinforced with boron-epoxy / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert J. Platt, Lewis B. Thurston, and Langley Research Center (page images at HathiTrust)
• Microgravity science and applications bibliography : 1991 revision / ([Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by United States. Office of Space Science and Applications and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
• Free vibrations of thin-walled semicircular graphite-epoxy composite frames / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Ahmed Khairy Noor, Jeanne M. Peters, Huey D. Carden, and Langley Research Center (page images at HathiTrust)
• A protection and detection surface (PADS) for damage tolerance / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Mark J. Shuart, Sherrill B. Biggers, Chunchu B. Prasad, and Lewis Research Center (page images at HathiTrust)
• Structural behavior of composite materials / (Washington : National Aeronautics and Space Administration : Springfield, Va. : for sale by the National Technical Information Service, 1964), by Stephen W. Tsai and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boron filaments / ([Washington, D.C.] : National Aeronautics and Space Administration, [1964]), by Robert M. Witucki, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of a metal shear web selectively reinforced with filamentary composites for space shuttle application / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by J. H. Laakso, J. W. Straayer, Langley Research Center, and Boeing Aerospace Company (page images at HathiTrust)
• Thermal-distortion analysis of an antenna strongback for geostationary high-frequency microwave applications / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Jeffery T. Farmer, Robert L. Wright, Deborah M. Wahls, and Langley Research Center (page images at HathiTrust)
• Thermal-distortion analysis of a spacecraft box truss in geostationary orbit / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Patrick A. Cosgrove, Lawrence F. Rowell, Jeffery T. Farmer, and Langley Research Center (page images at HathiTrust)
• A novel method of testing the shear strength of thick honeycomb composites / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1991), by A. J. Hodge, A. T. Nettles, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Dawn C. Jegley and Langley Research Center (page images at HathiTrust)
• An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1990), by A. T. Nettles, A. J. Hodge, D. G. Lance, and George C. Marshall Space Flight Center. Materials and Processes Laboratory (page images at HathiTrust)
• A lattice model for composite materials / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Theodore R. Tauchert, A. Cemal Eringen, T. Y. Chang, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by A. V. Viswanathan, L. L. Baker, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Minimum weight design of ring and stringer stiffeners for axially compressed cylindrical shells with and without internal pressure / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by David L. Block, Langley Research Center, and Florida Technological University (page images at HathiTrust)
• Two bonded half planes with a crack going through the interface / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by F. Erdogan, V. Biricikoglu, Langley Research Center, and Lehigh University (page images at HathiTrust)
• Wave surfaces due to impact on anisotropic fiber composite plates / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by F. C. Moon, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jerrold M. Housner, Manuel Stein, and Langley Research Center (page images at HathiTrust)
• Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by A. V. Viswanathan, R. E. Miller, Tsai-Chen Soong, Langley Research Center, and Boeing Company (page images at HathiTrust)
• Tensile failure criteria for fiber composite materials / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1972), by B. Walter Rosen, Carl H. Zweben, and Materials Sciences Corporation (page images at HathiTrust)
• Holographic nondestructive tests performed on composite samples of ceramic-epoxy-fiberglass sandwich structure / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert L. Kurtz, George C. Marshall Space Flight Center. Space Sciences Laboratory, and Hsun Kao Liu (page images at HathiTrust)
• Some metal-graphite and metal-ceramic composites for use as high-energy brake lining materials / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert C. Bill and Lewis Research Center (page images at HathiTrust)
• Graphite-polyimide composite for application to aircraft engines / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Morgan P. Hanson, C. C. Chamis, and Lewis Research Center (page images at HathiTrust)
• Minimum-weight designs for hat-stiffened composite panels under uniaxial compression / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Banarsi Agarwal, Randall C. Davis, and Langley Research Center (page images at HathiTrust)
• The effect of interfiber distance and temperature on the critical aspect ratio in composites / (Washington, DC : National Aeronautics and Space Administration, 1968), by Robert W. Jech, Robert A. Signorelli, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A computerized symbolic integration technique for development of triangular and quadrilateral composite shallow-shell finite elements / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Carl M. Andersen, Ahmed Khairy Noor, and Langley Research Center (page images at HathiTrust)
• Cyclic debonding of unidirectional composite bonded to aluminum sheet for constant-amplitiude loading / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1976), by George L. Roderick, John H. Crews, Richard A. Everett, and Langley Research Center (page images at HathiTrust)
• Composite materials / (Washington, D.C. : Science Reference Section, Science and Technology Division, Library of Congress, 1986), by George D. Havas and Library of Congress. Science and Technology Division. Reference Section (page images at HathiTrust)
• Development of quality assurance methods for epoxy graphite prepreg / (Washington, D.C. : National Aeronautics and Space Adminstration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by J. S. Chen, A. B. Hunter, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Boeing Commercial Airplane Company, and Langley Research Center (page images at HathiTrust)
• Composite panels made with biofiber or office wastepaper bonded with thermoplastic and/or thermosetting resin / (Madison, WI : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, [2004]), by James H. Muehl, Poo Chow, A. Krzysik, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• MFPG : advanced composites : design and applications : proceedings of the 29th meeting of the Mechanical Failures Prevention Group, held at the National Bureau of Standards, Gaithersburg, Maryland, May 23-25, 1979 /, by Mechanical Failures Prevention Group, William A. Willard, T. R. Shives, and Center for Materials Science (National Measurement Laboratory) (page images at HathiTrust)
• Composite materials for offshore operations : proceedings of the first International Workshop, Houston, Texas, October 26-28, 1993 / ([Boulder, CO] : U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology ; Washington, DC : For sale by the Supt. of Docs., U.S. G.P.O., [1995]), by Tex.) International Workshop on Composite Materials for Offshore Operations (1st : 1993 : Houston, Dale W Fitting, S. S Wang, and National Institute of Standards and Technology (U.S.) (page images at HathiTrust)
• Environmental exposure effects on composite materials for commercial aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Martin N. Gibbins, Daniel J. Hoffman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Selected NASA research in composite materials and structures. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Wash.) Industry Review of the NASA Aircraft Energy Efficiency Composite Programs (2nd : 1980 : Seattle, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Impact damage characterization and damage tolerance of composite sandwich airframe structures / [John S. Tomblin ... et al.] (Washington, D.C. : Office of Aviation Research, U.S. Federal Aviation Administration ; [Springfield, Va. : Available through the National Technical Information Service, 2001]), by John S. Tomblin, Wichita State University. Department of Aerospace Engineering, William J. Hughes Technical Center (U.S.), and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Lightning simulation test technique evaluation / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1988]), by William W. Cooley, Deborah L. Shortess, Inc Science & Engineering Associates, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Evaluations of filament-reinforced composites for aerospace structural applications / ([Washington] National Aeronautics and Space Administration, [1964]), by Norris F. Dow, B. Walter Rosen, General Electric Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Response and failure of composite plates with a bolt-filled hole / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1998]), by U. M. Yan, Stanford University. Department of Aeronautics and Astronautics, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Graphite/Polyimide composites / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by John G. Davis, H. Benson Dexter, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and CASTS Project Technical Symposium (1979 : Langley Research Center) (page images at HathiTrust)
• Issues related to the use of, and exposure to, various chemicals : hearings before the Subcommittee on Toxic Substances, Environmental Oversight, Research and Development of the Committee on Environment and Public Works, United States Senate, One Hundred First Congress, first session, March 6, 1989; July 5, 1989--Los Angeles, CA. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1989), by Environmental Oversight United States. Congress. Senate. Committee on Environment and Public Works. Subcommittee on Toxic Substances (page images at HathiTrust)
• NR-150B2 adhesive development / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by P. S. Blatz, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Application of In Situ Fiberization for fabrication of improved strain isolation pads and graphite-epoxy composites / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by R. W. Rosser, D. I. Basiulis, R. W. Seibold, Hughes Aircraft Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Health hazards of combustion products from aircraft composite materials / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by Sanjeev Gandhi, Richard E. Lyon, Galaxy Scientific Corporation, Federal Aviation Administration Technical Center (U.S.), and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Structural integrity evaluation of the Lear Fan 2100 aircraft / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by H. P. Kan, T. A. Dyer, Langley Research Center, Northrop Corporation. Military Aircraft Division, and United States. Office of Aviation Research (page images at HathiTrust)
• Effects of stiffener/rib separation on damage growth and residual strength / (Washington, DC : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by H. P. Kan, M. Mahler, Langley Research Center, Northrop Corporation. Military Aircraft Division, and United States. Office of Aviation Research (page images at HathiTrust)
• The Effect of preloading on fatigue damage in composite structures. (Washington, DC : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by H. Thomas Hahn, Los Angeles. Mechanical University of California, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Handbook : manufacturing advanced composite components for airframes / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1997]), by Terry L. Price, Cerritos College. Composites Training Ccenter, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Development of probabilistic design methodology for composite structures / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1997]), by P. M. Gary, M. G. Riskalla, Vought Aircraft Company, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Applications of fracture mechanics to the durability of bonded composite joints / (Washington, D.C.: Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1998]), by W. S. Johnson, Rodolfo V. Valentin, Lawrence M. Butkus, George W. Woodruff School of Mechanical Engineering, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Advanced certification methodology for composite structures / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1997]), by H. P. Kan, R. S. Whitehead, R. Cordero, Naval Air Warfare Center (U.S.), Northrop Corporation. Aircraft Division, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Enhanced reliability prediction methodology for impact damaged composite structures / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1998]), by H. P. Kan, Northrop Corporation. Military Aircraft Systems Division, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Comparative evaluation of failure analysis methods for composite laminates / (Washington, D.C. : Federal Aviation Administration Administration, Office of Aviation Research : Springfield, Va. : Available through the National Technical Information Service, [1996]), by C. T. Sun, Galaxy Scientific Corporation, Purdue University. School of Aeronautics and Astronautics, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• A predictive methodology for delamination growth in laminated composites. (Washington, D.C.: Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1998]), by Barry D. Davidson, Syracuse University. Department of Mechanical and Aerospace Engineering, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• The effect of loading parameters on fatigue of composite laminates. (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1997]), by H. Thomas Han, Seung Gyu Lim, Jonathan Bartley-Cho, Los Angeles. Mechanical and Aerospace Engineering Dept University of California, Federal Aviation Administration Technical Center (U.S.), and United States. Office of Aviation Research (page images at HathiTrust)
• Test methods for composites : a status report / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Inforamtion Service, [1993]), by S. Chaterjee, Donald W. Oplinger, D. Adams, U.S. Army Research Laboratory, University of Wyoming. Composite Materials Research Group, Materials Science Corporation, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Crashworthiness and scaling issues in using composite materials for guardrail applications / (McLean, Va. : Federal Highway Administration ; [Springfield, Va. : Available through the National Technical Information Service, 1995]), by Alrik L. Svenson and United States. Federal Highway Administration (page images at HathiTrust)
• Carbon-carbon process variations / (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, U.S. Air Force, 1979), by General Electric Company. Re-entry and Environmental Systems Division and E.R. Stover (page images at HathiTrust)
• Mechanics of composite materials (Wright-Patterson Air Force Base, Ohio, Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, 1966-), by Stephen W. Tsai (page images at HathiTrust)
• A survey of the literature on the size effect on material strength / (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1977), by H. Leon Harter and Air Force Flight Dynamics Laboratory (U.S.) Structural Mechanics Division (page images at HathiTrust)
• Advanced composite structures. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1974) (page images at HathiTrust)
• Compilation of radiation damage test data = Index des résultats d'essais de radiorésistance / (Geneva : CERN, European Organization for Nuclear Research, <1998-2001>), by M. Tavlet, H. Schönbacher, A. Fontaine, and European Organization for Nuclear Research (page images at HathiTrust)
• Compressive instability and strength of uniaxial filament-reinforced epoxy tubes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by John G. Davis, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Composite materials, the influence of mechanics of failure on design : proceedings of the Army Symposium on Solid Mechanics, 1976. (Watertown, Mass. : Army Materials and Mechanics Research Center, 1976), by Mass.) Army Symposium on Solid Mechanics (5th : 1976 : Bass River and Army Materials and Mechanics Research Center (U.S.) (page images at HathiTrust; US access only)
• Two-phase hydrogen density measurements using an open-ended microwave cavity / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Jerry Smetana, Norman C. Wenger, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Fiber reinforcement in plastics / (Pullman, Wash. : Technical Extension Service, Washington State University, 1965), by R. A. V. Raff, Washington State University. Technical Extension Service, and Washington State University. Washington State Institute of Technology (page images at HathiTrust; US access only)
• Composite materials : a compilation / ([Washington] : NASA ; Springfield, Va. : for sale by the National Technical Information Service ;, 1975), by United States. National Aeronautics and Space Administration. Technology Utilization Office (page images at HathiTrust)
• Die Familie Vanderhouten / (Berlin : Morawe & Scheffelt, 1917), by Adele Gerhard (page images at HathiTrust; US access only)
• Failure analysis and mechanisms of failure of fibrous composite structures / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983), by Ahmed Khairy Noor, Joint Institute for Advancement of Flight Sciences, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, George Washington University, and Langley Research Center (page images at HathiTrust)
• Tough composite materials / (s.l. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984), by Louis A. Teichman, Norman J. Johnston, Louis F. Vosteen, and Tough Composite Materials Workshop (1983 : NASA Langley Research Center) (page images at HathiTrust)
• Experimental data on single-bolt joints in quasi-isotropic graphite/polyimide laminates / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), by Gregory R. Wichorek, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Preliminary structural design of composite main rotor blades for minimum weight / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Mark W. Nixon and United States. Army. Aerostructures Directorate (page images at HathiTrust)
• The effects of simulated space environmental parameters on six commercially available composite materials / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), by Joan G. Funk, George F. Sykes, and United States. National Aeronautics and Space Administration. Office of Management (page images at HathiTrust)
• Tungsten fiber reinforced copper matrix composites : a review / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by David L. McDanels and Lewis Research Center (page images at HathiTrust)
• Evaluation of selected thermal control coatings for long-life space structures / ([Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Louis A. Teichman, William G. Witte, Wayne S. Slemp, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Environmental effects on composites for aircraft / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office, 1978), by Richard A. Pride and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Toughening of graphite-expoxy composites by interlaminar preforated Mylar films / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Wolf Elber and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Pocketing mechanics of SRM nozzle liner / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by V. Verderaime and George C. Marshall Space Flight Center (page images at HathiTrust)
• Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Gregory R. Wichorek, John H. Crews, and Langley Research Center (page images at HathiTrust)
• INHYD computer code for intraply hybrid composite design : users manual / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by C. C. Chamis, John H. Sinclair, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A repair technology program at NASA on composite materials / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Jerry W. Deaton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analytical study of effects of surface and environmental thermal properties on moisture in composites. (Washington : National Aeronautics and Space Administration ;, 1977), by Stephen S. Tompkins (page images at HathiTrust)
• An integrated computer procedure for sizing composite airframe structures / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Jaroslaw Sobieszczanski-Sobieski, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1989), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
• A three-node C ̊element for analysis of laminated composite sandwich shells / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1989), by C. Wayne Martin, K. K. Gupta, and S. F. Lung (page images at HathiTrust)
• Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1990), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
• Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by C. A. Bigelow and Langley Research Center (page images at HathiTrust)
• Failure mechanics in low-velocity impacts on thin composite plates / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Wolf Elber and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by John H. Crews, I. S. Raju, C. S. Hong, Joint Institute for Advancement of Flight Sciences, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of static tensile load on the thermal expansion of Gr/PI composite material / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Gary L. Farley, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by P. Daniel Sydow, Mark J. Shuart, and Langley Research Center (page images at HathiTrust)
• Optimization of composite sandwich cover panels subjected to compressive loadings / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Juan R. Cruz and Langley Research Center (page images at HathiTrust)
• Investigation of thermal fatigue in fiber composite materials / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Abdel A. Fahmy, Thomas G. Cunningham, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Richard L. Bielawa, United Technologies Research Center, United States National Aeronautics and Space Administration, Langley Research Center, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)
• Physical properties of thin films / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1972]), by Peter R. Preiswerk, M. E. Lippman, United States National Aeronautics and Space Administration, and Astro Research Corporation (page images at HathiTrust)
• Preliminary investigation of crack arrest in composite laminates containing buffer strips / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by J. G. Goree and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Radiation testing of composite materials, in situ versus ex situ effects / (Washington, D.C. : National Aeronautics and Space Administration, Scietific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 1981]), by Richard M. Kurland, William C. Beggs, James F. Thomasson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and TRW Defense and Space Systems Group (page images at HathiTrust)
• Theoretical studies of radiation effects on composite materials for space use / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by C. Ken Chang, Efstathios Kamaratos, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Designing for impact resistance with unidirectional fiber composites [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by C. C. Chamis, Tito T. Serafini, Morgan P. Hanson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical buckling loads of boron/aluminum and graphite/resin fiber-composite anisotropic plates / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 22151], 1971), by C. C. Chamis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Establishing allowable temperature gradients for tungsten-uranium dioxide fuel elements using experimental cyclic strain data / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Ivan B. Fiero and Lewis Research Center (page images at HathiTrust)
• Properties of three graphite/toughened resin composites / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Donald L. Smith, Marvin B. Dow, and Langley Research Center (page images at HathiTrust)
• Microgravity science and applications program tasks / ([Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991), by United States. Office of Space Science and Applications and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Moisture determination in composite materials using positron lifetime technique / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Jag J. Singh, Willis Mock, William H. Holt, Naval Surface Weapons Center, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Noise transmission loss of a rectangular plate in an infinite baffle / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Louis A. Roussos and Langley Research Center (page images at HathiTrust)
• Long-term thermal aging of two graphite/polyimide composite materials / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1984), by James B. Nelson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Fracture toughness of fibrous composite materials / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by C. C. Poe and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Delamination stresses in semicircular laminated composite bars / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by William L. Ko and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Evaluation of composite components on the Bell 206L and Sikorsky S-76 helicopters / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Donald J. Baker and United States. Army Aerostructures Directorate (page images at HathiTrust)
• Vibration testing of impact-damaged composite laminates / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Joseph H. Grady and Erwin H. Meyn (page images at HathiTrust)
• Buckling and structural efficiency of sandwich-blade stiffened composite compression panels / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Manuel Stein, Jerry G. Williams, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Stress-concentration factors for finite orthotropic laminates with a circular hole and uniaxial loading / (Washington, D.C. : National Aeronautics and Space Administration, Scientifice and Technical Information Office [Springfield, Va. : For sale by the National Technical Information Service], 1979), by C. S. Hong, John H. Crews, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Elevated-temperature application of the IITRI compression test fixture for graphite/polyimide filmentary composites / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by B. Basava Raju, Paul A. Cooper, Charles J. Camarda, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moisture diffusion parameter characteristics for epoxy composites and neat resins / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Edward R. Long, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Microgravity science and applications bibliography : 1989 revision / ([Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990), by United States. Office of Space Science and Applications and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Exploratory investigation of two resin-matrix composites subjected to arc-tunnel heating / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by C. M. Pittman, Ronald D. Brown, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Zero thermal expansion composites of high strength and stiffness / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Norris F. Dow, B. Walter Rosen, Langley Research Center, and General Electric Company (page images at HathiTrust)
• Finite element computer program to analyze cracked orthotropic sheets / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by C. S. Chu, United States National Aeronautics and Space Administration, and Lockheed-Georgia Company (page images at HathiTrust)
• Fundamental analysis of the failure of polymer-based fiber reinforced composites / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by M. F. Kanninen, Battelle Memorial Institute, and Ames Research Center (page images at HathiTrust)
• The effect of configuration on strength, durability, and handle of Kevlar fabric-based materials / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Service, 1977), by L. L. Rueter, J. B. Munson, Inc Sheldahl, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of Kevlar fabric-based materials for use with inflatable structures / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by R. J. Niccum, L. L. Rueter, J. B. Munson, Inc Sheldahl, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by A. V. Viswanathan, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Mathematical modeling of damage in unidirectional composites / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by J. G. Goree, Walter F. Jones, Lokeswarappa R. Dharani, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Shear-lag analysis of a hybrid, unidirectional composite with fiber damage / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by J. G. Goree, Lokeswarappa R. Dharani, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A Study of the stress wave factor technique for the characterization of composite materials / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Edmund G. Henneke, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Development of new addition-type composite resins / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by R. J. Kray, CIBA-GEIGY Corporation, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Experimental determination of the effects of moisture on composite-to-composite adhesive joints / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Richard J. DeIasi, Robert L. Schulte, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of fiber/matrix interactions on the properties of graphite/epoxy composites / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Paul E. McMahon, Lincoln Ying, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Celanese Corporation, and Langley Research Center (page images at HathiTrust)
• Deformation measurements of composite multi-span beam shear specimens by moire interferometry / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Daniel Post, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Glass-, boron-, and graphite-filament-wound resin composites and liners for cryogenic pressure vessels / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Morgan P. Hanson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of three liquid-metal quality measurement techniques / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Ted W. Nyland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and theoretical investigation of the ablative performance of five phenolic-nylon-based materials / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Allen G. McLain, Gerald D. Walberg, Kenneth Sutton, and Langley Research Center (page images at HathiTrust)
• Tensile behavior of unnotched and notched tungsten-copper laminar composites / (Washington : National Aeronautics and Space Administration ; Springfield, Va. for sale by the National Technical Information Service, 1976), by Charles A. Hoffman, John W. Weeton, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Rim-spoke composite flywheels : stress and vibration analysis / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by C. C. Chamis, Louis J. Kiraly, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Failure criteria for filamentary composites / (Washington, DC : National Aeronautics and Space Administration, 1969), by Christos Chamis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of thermal and environmental exposure on the mechanical properties of graphite/polyimide composites / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by M. P. Hanson, T. T. Serafini, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effects of thermal loading on composites with constituents of differing thermal expansion / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Charles A. Hoffman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of three classes of composite materials for space vehicle application / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by John A. Alexander, B. A. Macklin, and J. C. Withers (page images at HathiTrust; US access only)
• Fire smoke and toxicity of composites on high speed craft / (Washington, DC : U.S. Coast Guard, Marine Safety and Environmental Protection ; Springfield, Va. : Available through the National Technical Information Service, [1998]), by Marc L. Janssens, Leigh Orvis, Southwest Research Institute, U.S. Coast Guard Research & Development Center, and United States. Coast Guard. Marine Safety and Environmental Protection (page images at HathiTrust)
• Impact characteristics of glass fiber-reinforced composite materials for use in roadside safety barriers / (McLean, Va. : Federal Highway Administration ; [Springfield, Va. : Available through the National Technical Information Service, 1994]), by Alrik L. Svenson and United States. Federal Highway Administration (page images at HathiTrust)
• Delamination of kaolin by high-energy, ionizing radiation / (Atlanta, Ga. : Engineering Experiment Station, Georgia Institute of Technology, 1961), by William J. Corbett, John H. Burson, U.S. Atomic Energy Commission. Savannah River Operations Office, U.S. Atomic Energy Commission, and Georgia Institute of Technology. Engineering Experiment Station (page images at HathiTrust)
• Advanced composites : design and applications : proceedings of the 29th meeting of the Mechanical Failures Prevention Group, held at the National Bureau of Standards, Gaithersburg, Maryland, May 23-25, 1979 / (Washington, D.C. : U.S. Dept. of Commerce, National Bureau of Standards, 1979), by Mechanical Failures Prevention Group. Meeting (29th : 1979 : National Bureau of Standards), William A. edt Willard, T. R. edt Shives, United States. National Bureau of Standards. Special publication, and Center for Materials Science (National Measurement Laboratory) (page images at HathiTrust)
• Concrete-polymer materials : first topical report / (Upton, N.Y. : Brookhaven National Laboratory ; Springfield, Va. : Clearinghouse for Federal Scientific and Technical Information, National Bureau of Standards, U.S. Dept. of Commerce, 1968), by Meyer Steinberg, United States. Office of Saline Water, U.S. Atomic Energy Commission. Division of Isotopes Development, United States. Bureau of Reclamation. Denver Office. Division of Research, and Brookhaven National Laboratory. Department of Nuclear Engineering (page images at HathiTrust)
• Investigation of a corrugated shell as an elastic support of a bundle of rods / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation, 1961), by J. H. Meier, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The elastic-plastic stresses within a tube generating internal heat uniformly / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation., 1961), by Bernard W. Shaffer, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Summary of the fifteenth refractory composites working group meeting / (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1969), by D. J Maykuth, K. R. Hanby, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Summary of the sixteenth refractory composites working group meeting / (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1969), by K. R Hanby, D. J. Maykuth, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Effect of fiber orientation on initial postbuckling behavior and imperfection sensitivity of composite cylindrical shells / (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by N. S. Khot, V. B. Venkayya, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Effect of service environment on F-15 boron/epoxy stabilator /, by T. V. Hinkle, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing body United States. Air Force. Systems Command, and sponsor McDonnell Douglas Corporation (page images at HathiTrust)
• Advanced fatigue damage development in graphite epoxy laminates /, by Russell D. Jamison, K. L. Reifsnider, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Performance concept in buildings : proceedings of a symposium jointly sponsored by the International Union of Testing and Research Laboratories for Materials and Structures (RILEM), the American Society for Testing and Materials (ASTM), and the International Council for Building Research Studies and Documentation (CIB), Philadelphia, Pa., May 2-5, 1972. (Washington, D.C. : U.S. Dept. of Commerce, National Bureau of Standards : U.S. Govt. Print Off., 1972), by United States. National Bureau of Standards. Special publication, Studies and Documentation International Council for Building Research, American Society for Testing and Materials, and International Union of Testing and Research Laboratories for Materials and Structures, ed. by Bruce Foster (page images at HathiTrust)
• Fabrication development of boron carbide and boron carbide+silicon carbide mixtures for possible application as lumped burnable poisons in PWR-2 /, by S. F. Kaufman, Westinghouse Electric Corporation, Bettis Atomic Power Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Summary of the Tenth Refractory Composites Working Group Meeting /, by L. N. Hjelm, Elvin H. Beardslee, Darrell R. James, and issuing agency Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Temperature responses of composite panels /, by Lit S. Han, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Ohio State University. Department of Mechanical Engineering (page images at HathiTrust)
• Advanced residual strength degradation rate modeling for advanced composite structures., by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Buckling of composites under hot and wet environment /, by V. Sarma Avva, L. Sharpe, D. Yogi Goswami, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor North Carolina Agricultural and Technical State University (page images at HathiTrust)
• Sonic fatigue design techniques for advanced composite aircraft structures : Final report /, by Ian Holehouse, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and Inc. Rohr Industries (page images at HathiTrust)
• Advanced residual strength degradation rate modeling for advanced composite structures., by D. E. Pettit, J. M. Cox, K. N. Lauraitis, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Revised instructions for TI-59 combined card/module calculations for in-plane and flexural properties of symmetric laminates /, by Steven L. Donaldson and sponsor Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Summary of the Thirteenth Refractory Composites working group meeting /, by Elvin H. Beardslee and issuing agency Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Advanced residual strength degradation rate Modeling for advanced composite structures., by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• The relationship between tensile strength and flexure strength in fiber reinforced composites /, by James Martin Whitney, Marvin Knight, issuing agency Air Force Wright Aeronautical Laboratories, and sponsor Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Properties of organic matrix short fiber composites /, by George S. Springer, Rodney L. Clark, Algirdas Maciulaitis, sponsor Air Force Wright Aeronautical Laboratories, and sponsor University of Michigan. Department of Mechanical Engineering & Applied Mechanics (page images at HathiTrust)
• Investigation of techniques and materials for the formation of high temperature (1500 F) inorganic fiber /, by Richard B. Ellis, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. sponsor, and Ala.) Southern Research Institute (Birmingham (page images at HathiTrust)
• Transient heat flow across unidirectional fibers in composites /, by Lit S. Han, Moshen Bashizadeh-Fakhar, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Effects of fighter attack spectrum on composite fatigue life /, by R. Badaliance, H. D. Dill, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor McDonnell Aircraft Company (page images at HathiTrust)
• Matrix-dominated time-dependent deformation and damage of graphite epoxy composite experimental data under ramp loading /, by Edward M. Wu, Nhan Q. Nguyen, Richard L Moore, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Lawrence Livermore National Laboratory (page images at HathiTrust)
• Evaluation of sapphire wool and its incorporation into composites of high strength /, by R. L. Mehan, A. Gatti, Earl Feingold, issuing agency Air Force Materials Laboratory (U.S.), and sponsor General Electric Company. Space Sciences Laboratory (page images at HathiTrust)
• Investigation of nondestructive methods for the evaluation of graphite materials /, by R. C. Stinebring, J. W. Orner, A. W. Schultz, issuing agency Air Force Materials Laboratory (U.S.), and sponsor Avco Corporation (page images at HathiTrust)
• Instructions for TI-59 combined card/module calculations for in-plane properties of symmetric hybrid laminates /, by Stella D. Gates and sponsor Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Optimum filament wound composites /, by G. P. Peterson, issuing agency United States. Air Force. Systems Command, and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Mechanics of composite materials., by Stephen W. Tsai, sponsor Air Force Materials Laboratory (U.S.), and issuing agency United States. Air Force. Systems Command (page images at HathiTrust)
• Proceedings of the 1982 Joint Conference on Experimental Mechanics, Oahu-Maui, Hawaii, May 23-28. (Brookfield Center, CT. : Society for Experimental Stress Analysis, c1982), by Hawaii) Joint Conference on Experimental Mechanics (1982 : Oahu-Maui, Nihon Kikai Gakkai, and Society for Experimental Stress Analysis (page images at HathiTrust; US access only)
• BUCKDEL v 0.9 users and theory manuals : buckling and delamination analysis of stiffened laminated plates /, by Daniel S. Pipkins, Satya N. Atluri, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Implementation of a damage tolerance module into ASTROS /, by Daniel S. Pipkins, Satya N. Atluri, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Impact damage tolerance of composites exposed to hot, cold and wet environments /, by V. Sarma Avva, sponsor North Carolina Agricultural and Technical State University, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Wright Research and Development Center, and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Fatigue/impact studies in laminated composites /, by V. Sarma Avva, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor North Carolina Agricultural and Technical State University (page images at HathiTrust)
• Improved materials for composites and adhesive joints /, by Ronald A. Servais, S. Soni, M. Rich, M. Koenig, R. Kim, J. Hartness, W. Click, H. Chai, D. Anderson, issuing body Air Force Wright Aeronautical Laboratories, and sponsor University of Dayton. Research Institute (page images at HathiTrust)
• Adhesive strip concept for delamination arrestment /, by James R. Eisenmann, David A. Ulman, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Design methodology and life analysis of postbuckled metal and composite panels., by Ravi B. Deo, Erdogan Madenci, B. L. Agarwal, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Metal fiber reinforced ceramics., by James Root Tinklepaugh, D. D. Button, J. H. Connor, W. R. Hoskyns, B. R. Goss, United States. Air Force. Air Research and Development Command. issuing body, sponsor Air Force Materials Laboratory (U.S.), and sponsor New York State College of Ceramics at Alfred University (page images at HathiTrust)
• Matrix-dominated time-dependent deformation and damage of graphite-epoxy composite : experimental data under multiple-step relaxation /, by Edward Ming-chi Wu, Richard L. Moore, Nhan Q. Nguyen, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lawrence Livermore National Laboratory (page images at HathiTrust)
• Design Methodology and Life Analysis of Postbuckled Metal and Composite Panels: Design Guide. Volume III /, by Ravi B. Deo, B. L. Agarwal, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Design development and durability validation of postbuckled composite and metal panels: technology assessment /, by Ravi B. Deo, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Metal fiber reinforced ceramics., by J. J. Swica, James Root Tinklepaugh, J. H. Connor, B. R. Goss, W. R. Hoskyns, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, sponsor Air Force Materials Laboratory (U.S.), and sponsor New York State College of Ceramics at Alfred University (page images at HathiTrust)
• Metal fiber reinforced ceramics., by R. S. Truesdale, James Root Tinklepaugh, J. J. Swica, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, sponsor Air Force Materials Laboratory (U.S.), and sponsor New York State College of Ceramics at Alfred University (page images at HathiTrust)
• Horizontal shear testing of woven fiberglass/epoxy composites /, by Robert T. Achard, issuing body Air Force Wright Aeronautical Laboratories, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)

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