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Composite materials -- Mathematical models

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• Composite materials
• Materials -- Mathematical models
• Mathematical models

• Composite materials -- Computer simulation
• Fibrous composites -- Mathematical models
• Laminated materials -- Mathematical models
• Metallic composites -- Mathematical models
• Composite materials -- Bonding -- Mathematical models
• Composite materials -- Delamination -- Mathematical models
• Composite materials -- Fatigue -- Mathematical models
• Composite materials -- Noise -- Mathematical models

• A three-node C ̊element for analysis of laminated composite sandwich shells (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by C. Wayne Martin, K. K. Gupta, and S. F. Lung (page images at HathiTrust)
• Moisture diffusion parameter characteristics for epoxy composites and neat resins (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites (National Aeronautics and Space Administration ;, 1971), by A. V. Viswanathan, R. E. Miller, Tsai-Chen Soong, Langley Research Center, and Boeing Company (page images at HathiTrust)
• Fundamental analysis of the failure of polymer-based fiber reinforced composites (U.S. National Aeronautics and Space Administration ;, 1976), by M. F. Kanninen, Battelle Memorial Institute, and Ames Research Center (page images at HathiTrust)
• Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads (National Aeronautics and Space Administration ;, 1974), by A. V. Viswanathan, L. L. Baker, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 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)

• Rim-spoke composite flywheels : stress and vibration analysis (National Aeronautics and Space Administration ;, 1976), by C. C. Chamis, Louis J. Kiraly, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Minimum-weight designs for hat-stiffened composite panels under uniaxial compression (National Aeronautics and Space Administration ;, 1974), by Banarsi Agarwal, Randall C. Davis, and Langley Research Center (page images at HathiTrust)

• Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels (National Aeronautics and Space Administration ;, 1975), by Jerrold M. Housner, Manuel Stein, and Langley Research Center (page images at HathiTrust)
• Minimum-mass design of filamentary composite panels under combined loads : design procedure based on a rigorous buckling analysis (National Aeronautics and Space Administration ;, 1977), by W. Jefferson Stroud, Melvin S. Anderson, Nancy Agranoff, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• A finite-difference program for stresses in anisotropic, layered plates in bending (National Aeronautics and Space Administration ;, 1975), by Nicholas J. Salamon and George C. Marshall Space Flight Center. Structures and Propulsion Laboratory (page images at HathiTrust)
• A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle (National Aeronautics and Space Administration ;, 1974), by J. A. Sova, John H. Crews, and Langley Research Center (page images at HathiTrust)

• LamLum : a tool for evaluating the financial feasibility of laminated lumber plants (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 2006), by Edward M. Bilek, John Hunt, and Forest Products Laboratory (U.S.) (page images at HathiTrust)

• A method for determining local elastoplastic stress and strain in metallurgically bonded notched laminates subjected to a loading cycle (National Aeronautics and Space Administration ;, 1974), by J. A. Sova, John H. Crews, and Langley Research Center (page images at HathiTrust)

• A computerized symbolic integration technique for development of triangular and quadrilateral composite shallow-shell finite elements (National Aeronautics and Space Administration ;, 1975), by Carl M. Andersen, Ahmed Khairy Noor, and Langley Research Center (page images at HathiTrust)

• A cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by C. A. Bigelow and Langley Research Center (page images at HathiTrust)
• Effect of measured material properties on the finite element analysis of an OH-58 composite tail boom (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Lynn M. Bowman and United States. Army. Aerostructures Directorate (page images at HathiTrust)
• Analytical study of rigidized fibrous materials (National Aeronautics and Space Administration ;, 1974), by B. Walter Rosen, John J. Kibler, Debal Bagchi, Langley Research Center, and Materials Sciences Corporation (page images at HathiTrust)
• Minimum-mass design of filamentary composite panels under combined loads : design procedure based on simplified buckling equations (National Aeronautics and Space Administration ;, 1976), by W. Jefferson Stroud, Nancy Agranoff, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of the three-point-bend test for materials with unequal tension and compression properties (National Aeronautics and Space Administration ;, 1974), by C. C. Chamis and Lewis Research Center (page images at HathiTrust)

• Analytical study of rigidized fibrous materials (National Aeronautics and Space Administration ;, 1974), by B. Walter Rosen, John J. Kibler, Debal Bagchi, Langley Research Center, and Materials Sciences Corporation (page images at HathiTrust)

• Buckling behavior of long symmetrically laminated plates subjected to combined loadings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
• A three-node C ̊element for analysis of laminated composite sandwich shells (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by C. Wayne Martin, K. K. Gupta, and S. F. Lung (page images at HathiTrust)
• Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads (National Aeronautics and Space Administration ;, 1974), by A. V. Viswanathan, L. L. Baker, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Sharp PC-1500 Pocket Computer solutions to composite materials formulas (Wright-Patterson Air Force Base, Ohio : Material Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982, 1982), by Won J. Park, Thierry N. Massard, Air Force Wright Aeronautical Laboratories, and Inc Universal Energy Systems (page images at HathiTrust)

• A three-node C ̊element for analysis of laminated composite sandwich shells (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by C. Wayne Martin, K. K. Gupta, and S. F. Lung (page images at HathiTrust)

• Buckling coefficients for sandwich cylinders of finite length under uniform external lateral pressure (U.S. Dept. of Agriculture, Forest Service Forest Products Laboratory, 1965), by Edward W. Kuenzi, G. H. Stevens, Billy Bohannan, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)

• Shear-flexible finite-element models of laminated composite plates and shells (National Aeronautics and Space Administration ;, 1975), by Ahmed Khairy Noor, Michael D. Mathers, and Langley Research Center (page images at HathiTrust)

• Diffusion analysis for two-phase metal-matrix composite (National Aeronautics and Space Administration :, 1976), by Darrel R. Tenney and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by C. A. Bigelow and Langley Research Center (page images at HathiTrust)

• A predictive methodology for delamination growth in laminated composites. Part I : Theoretical development and preliminary experimental results (Federal Aviation Administration, Office of Aviation Research ;, 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)

• Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by C. A. Bigelow and Langley Research Center (page images at HathiTrust)
• Two bonded half planes with a crack going through the interface (National Aeronautics and Space Administration ;, 1973), by F. Erdogan, V. Biricikoglu, Langley Research Center, and Lehigh University (page images at HathiTrust)

• Noise transmission loss of a rectangular plate in an infinite baffle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Louis A. Roussos 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)
• Tensile strength of composite truss lumber as affected by veneer species and member width (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 (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 (U.S. Forest Products Laboratory, 1973), by John J. Zahn and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Composite panels made with biofiber or office wastepaper bonded with thermoplastic and/or thermosetting resin (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)
• Advanced composite structures. (National Aeronautics and Space Administration ;, 1974) (page images at HathiTrust)
• Mechanics of composite materials (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 (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)
• Composite materials : a compilation (NASA ;, 1975), by United States. National Aeronautics and Space Administration. Technology Utilization Office (page images at HathiTrust)
• Preliminary structural design of composite main rotor blades for minimum weight (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Mark W. Nixon and United States. Army. Aerostructures Directorate (page images at HathiTrust)
• Thermal-distortion analysis of an antenna strongback for geostationary high-frequency microwave applications (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 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 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Patrick A. Cosgrove, Lawrence F. Rowell, Jeffery T. Farmer, and Langley Research Center (page images at HathiTrust)
• Microgravity science and applications program tasks (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)
• Microgravity science and applications bibliography : 1991 revision (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)
• Toughening of graphite-expoxy composites by interlaminar preforated Mylar films (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Wolf Elber and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Delamination stresses in semicircular laminated composite bars (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)
• A repair technology program at NASA on composite materials (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Jerry W. Deaton and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An integrated computer procedure for sizing composite airframe structures (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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)
• Buckling and structural efficiency of sandwich-blade stiffened composite compression panels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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)
• Microgravity science and applications bibliography : 1989 revision (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 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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)
• Experimental data on single-bolt joints in quasi-isotropic graphite/polyimide laminates (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)
• Failure mechanics in low-velocity impacts on thin composite plates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 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)
• Optimization of composite sandwich cover panels subjected to compressive loadings (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)
• Boron filaments (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)
• A lattice model for composite materials (National Aeronautics and Space Administration ;, 1969), by Theodore R. Tauchert, A. Cemal Eringen, T. Y. Chang, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Zero thermal expansion composites of high strength and stiffness (National Aeronautics and Space Administration ;, 1969), by Norris F. Dow, B. Walter Rosen, Langley Research Center, and General Electric Company (page images at HathiTrust)
• Investigation of thermal fatigue in fiber composite materials (U.S. National Aeronautics and Space Administration ;, 1976), by Abdel A. Fahmy, Thomas G. Cunningham, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Investigation of three classes of composite materials for space vehicle application (National Aeronautics and Space Administration, 1967), by John A. Alexander, B. A. Macklin, and J. C. Withers (page images at HathiTrust)
• Finite element computer program to analyze cracked orthotropic sheets (U.S. National Aeronautics and Space Administration ;, 1976), by C. S. Chu, United States National Aeronautics and Space Administration, and Lockheed-Georgia Company (page images at HathiTrust)
• Evaluation of a metal shear web selectively reinforced with filamentary composites for space shuttle application (National Aeronautics and Space Administration ;, 1974), by J. H. Laakso, J. W. Straayer, Langley Research Center, and Boeing Aerospace Company (page images at HathiTrust)
• Development of lightweight aluminum compression panels reinforced by boron-epoxy infiltrated extrusions (National Aeronautics and Space Administration ;, 1973), by Paul A. Roy, Jim Henshaw, John A. McElman, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Development of quality assurance methods for epoxy graphite prepreg (National Aeronautics and Space Adminstration, Scientific and Technical Information Branch ;, 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)
• NR-150B2 adhesive development (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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)
• Shear-lag analysis of a hybrid, unidirectional composite with fiber damage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Application of In Situ Fiberization for fabrication of improved strain isolation pads and graphite-epoxy composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Theoretical studies of radiation effects on composite materials for space use (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Deformation measurements of composite multi-span beam shear specimens by moire interferometry (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Daniel Post, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• NASA TN D-4412 (National Aeronautics and Space Administration ;, 1968), by Morgan P. Hanson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4038 (National Aeronautics and Space Administration ;, 1967), by Ted W. Nyland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Tensile behavior of unnotched and notched tungsten-copper laminar composites (National Aeronautics and Space Administration ;, 1976), by Charles A. Hoffman, John W. Weeton, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-5926 (National Aeronautics and Space Administration :, 1970), by Charles A. Hoffman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5697 (National Aeronautics and Space Administration :, 1970), by John G. Davis, Langley 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 (National Aeronautics and Space Administration ;, 1971), by C. C. Chamis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Flight and ground tests of a very-low-density elastomeric ablative material (National Aeronautics and Space Administration ;, 1972), by George C. Olsen, Andrew Chapman, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6212 (National Aeronautics and Space Administration ;, 1971), by Jerry Smetana, Norman C. Wenger, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Self-lubricating plasma-sprayed composites for sliding-contact bearings to 900 ̊C (National Aeronautics and Space Administration ;, 1974), by Harold E. Sliney and Lewis Research Center (page images at HathiTrust)
• Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings (National Aeronautics and Space Administration ;, 1974), by Jerrold M. Housner, Manuel Stein, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6357 (National Aeronautics and Space Administration ;, 1971), by F. C. Moon, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Graphite-polyimide composite for application to aircraft engines (National Aeronautics and Space Administration ;, 1974), by Morgan P. Hanson, C. C. Chamis, and Lewis Research Center (page images at HathiTrust)
• Concrete-polymer materials : first topical report (Brookhaven National Laboratory ;, 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)
• Composite materials for rail transit systems (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)
• Interface control and mechnanical property improvements in silicon carbide/titanium composites (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by William D. Brewer, Jalaiah Unnum, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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 (National Aeronautics and Space Administration ;, 1967), by Donald A. Peterson and Lewis Research Center (page images at HathiTrust)
• The elastic-plastic stresses within a tube generating internal heat uniformly (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)
• Fiber reinforcement in plastics (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)
• Fabrication development of boron carbide and boron carbide+silicon carbide mixtures for possible application as lumped burnable poisons in PWR-2 (Washington, D.C. : Office of Technical Services, Department of Commerce, 1964., 1964), by S. F. Kaufman, Westinghouse Electric Corporation, Bettis Atomic Power Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Joining of advanced composites (Dept. of Defense], Dept. of the Army, Army Materiel Development and Readiness Command ;, 1979), by United States. Army Materiel Development and Readiness Command, Andrew Devine, and Plastics Technical Evaluation Center (U.S.) (page images at HathiTrust)
• Summary of the fifteenth refractory composites working group meeting (Defense Metals Information Center, Battelle Memorial Institute, 1969), by D. J. Maykuth, K. R. Hanby, and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Summary of the sixteenth refractory composites working group meeting (Defense Metals Information Center, Battelle Memorial Institute, 1969), by K. R Hanby, D. J. Maykuth, and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Impact damage characterization and damage tolerance of composite sandwich airframe structures / [John S. Tomblin ... et al.] (Office of Aviation Research, U.S. Federal Aviation Administration ;, 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)
• Response and failure of composite plates with a bolt-filled hole (Federal Aviation Administration, Office of Aviation Research ;, 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)
• The Effect of preloading on fatigue damage in composite structures. Part I (Federal Aviation Administration, Office of Aviation Research ;, 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)
• Development of probabilistic design methodology for composite structures (Federal Aviation Administration, Office of Aviation Research ;, 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)
• Advanced certification methodology for composite structures (Federal Aviation Administration, Office of Aviation Research ;, 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)
• The effect of loading parameters on fatigue of composite laminates. Part II (Federal Aviation Administration, Office of Aviation Research ;, 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)
• Effect of fiber orientation on initial postbuckling behavior and imperfection sensitivity of composite cylindrical shells (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 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by T. V. Hinkle, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and McDonnell Douglas Corporation (page images at HathiTrust)
• Optimum filament wound composites (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by G. P. Peterson, United States. Air Force. Systems Command, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Advanced fatigue damage development in graphite epoxy laminates (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Russell D. Jamison, K. L. Reifsnider, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Advanced residual strength degradation rate modeling for advanced composite structures. Volume 3. Appendixes to report for Tasks II and III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• Investigation of techniques and materials for the formation of high temperature (1500 F) inorganic fiber (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Richard B. Ellis, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and Ala.) Southern Research Institute (Birmingham (page images at HathiTrust)
• Mechanics of composite materials. Part I, Introduction (Wright-Patterson Air Force Base, Ohio, Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by Stephen W. Tsai, Air Force Materials Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Transient heat flow across unidirectional fibers in composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Lit S. Han, Moshen Bashizadeh-Fakhar, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Effects of fighter attack spectrum on composite fatigue life (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by R. Badaliance, H. D. Dill, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• Matrix-dominated time-dependent deformation and damage of graphite epoxy composite experimental data under ramp loading (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Edward M. Wu, Nhan Q. Nguyen, Richard L Moore, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Lawrence Livermore National Laboratory (page images at HathiTrust)
• Advanced residual strength degradation rate modeling for advanced composite structures. Volume 1. Task I: Preliminary screening (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by D. E. Pettit, J. M. Cox, K. N. Lauraitis, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• Evaluation of sapphire wool and its incorporation into composites of high strength (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by R. L. Mehan, A. Gatti, Earl Feingold, Air Force Materials Laboratory (U.S.), and General Electric Company. Space Sciences Laboratory (page images at HathiTrust)
• Investigation of nondestructive methods for the evaluation of graphite materials (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by R. C. Stinebring, J. W. Orner, A. W. Schultz, Air Force Materials Laboratory (U.S.), and Avco Corporation (page images at HathiTrust)
• Advanced residual strength degradation rate Modeling for advanced composite structures. Volume 2. Tasks II and III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• Fatigue/impact studies in laminated composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by V. Sarma Avva, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and North Carolina Agricultural and Technical State University (page images at HathiTrust)
• Adhesive strip concept for delamination arrestment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), by James R. Eisenmann, David A. Ulman, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Design methodology and life analysis of postbuckled metal and composite panels. Volume I (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Materials Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Ravi B. Deo, Erdogan Madenci, B. L. Agarwal, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Matrix-dominated time-dependent deformation and damage of graphite-epoxy composite : experimental data under multiple-step relaxation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Forc, 1983., 1983), by Edward Ming-chi Wu, Richard L. Moore, Nhan Q. Nguyen, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Lawrence Livermore National Laboratory (page images at HathiTrust)
• Design Methodology and Life Analysis of Postbuckled Metal and Composite Panels: Design Guide. Volume III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Materials Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Ravi B. Deo, B. L. Agarwal, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Design development and durability validation of postbuckled composite and metal panels: technology assessment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Ravi B. Deo, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Effects of fiber, matrix, and interphase on carbon fiber composite compression strength (National Aeronautics and Space Administration, Langley Research Center, 1994), by John A. Nairn, Willard D. Bascom, Sheila I. Harper, and Langley Research Center (page images at HathiTrust)
• Texcad-- textile composite analysis for design : version 1.0 user's manual (National Aeronautics and Space Administration ;, 1994), by Rajiv A. Naik, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips (National Aeronautics and Space Administration, Langley Research Center ;, 1995), by K. A. Yuan, Peretz Friedmann, Langley Research Center, and Los Angeles. Mechanical University of California (page images at HathiTrust)
• Structural evaluation of high strain fiber and resin composite material systems (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), by David L. Buchanan, Paul S. McClellan, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• Strain gage techniques for internal strain measurements in boron-epoxy composites (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by R. L. Egger, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Aerospace Company. Research and Engineering Division (page images at HathiTrust)
• HTMIAC newsletter (Center for Information and Numerical Data Analysis and Synthesis, Purdue University, in the 20th century), by Purdue University. Center for Information and Numerical Data Analysis and Synthesis and High Temperature Materials Information Analysis Center (U.S.) (page images at HathiTrust)

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