The Online Books Page

Superconducting composites

See also what's at your library, or elsewhere.

• Fibrous composites
• Metallic composites
• Superconductors

• Composite superconductors
• Superconducting composite materials

• Au Fe vs Cu thermocouples (Ames Laboratory, 1964), by D. K. Finnemore, T. F. Stromberg, J. E. Ostenson, U.S. Atomic Energy Commission, and Ames Laboratory (page images at HathiTrust)

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

• Implementation of a bond model, including dilation, for reinforced materials in a finite element analysis (Naval Facilities Engineering Service Center, 1996), by Joseph D. Mello, Leonard R. Herrmann, and Calif.) Naval Facilities Engineering Service Center (Port Hueneme (page images at HathiTrust)
• Critical aspect ratio for tungsten fibers in copper-nickel matrix composites (National Aeronautics and Space Administration ;, 1975), by Robert W. Jech and Lewis Research Center (page images at HathiTrust)
• Bonding and compatibility of aluminum oxide fibers in nickel alloy composites (National Aeronautics and Space Administration ;, 1976), by Leonard J. Westfall and Lewis Research Center (page images at HathiTrust)
• Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites (National Aeronautics and Space Administration ;, 1971), by S. Oken, Langley Research Center, Boeing Commercial Airplane Company, Boeing Company, and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• Spinning filamentary disk (National Aeronautics and Space Administration, 1964), by A. C. Kyser, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hollow multipartitioned ceramic structures (National Aeronautics and Space Administration, 1964), by William J. Eakins, Richard A. Humphrey, Inc DeBell and Richardson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Model for flaw-induced fracture in non-ductile materials (National Aeronautics and Space Administration, 1966), by H. U. Schuerch, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Carbide coated fibers in graphite-aluminum composites : progress report (National Aeronautics and Space Administration ;, 1975), by Richard J. Imprescia, Langley Research Center, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Ultrasonic characterization of the nonlinear elastic properties of unidirectional graphite/epoxy composites (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), by William H. Prosser (page images at HathiTrust)
• In situ polymerization of monomers for polyphenylquinoxaline-graphite fiber composites (National Aeronautics and Space Administration ;, 1974), by Tito T. Serafini, Raymond D. Vannucci, Peter Delvigs, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6463 (National Aeronautics and Space Administration ;, 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)
• NASA TN D-6146 (National Aeronautics and Space Administration ;, 1971), by C. C. Chamis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Characterization and design mechanics for fiber-reinforced metals (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by C. C. Chamis (page images at HathiTrust; US access only)
• 10 ̊off-axis tensile test for intralaminar shear characterization of fiber composites (National Aeronautics and Space Administration ;, 1976), by C. C. Chamis, John H. Sinclair, 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; US access only)
• High-temperature strength of refractory-metal wires and consideration for composite applications (National Aeronautics and Space Administration ;, 1972), by Donald W. Petrasek and Lewis Research Center (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)
• NASA TN D-4475 (National Aeronautics and Space Administration ;, 1968), by Charles P. Blankenship, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design properties of randomly reinforced fiber composites (NASA ;, 1972), by C. C. Chamis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3886 (National Aeronautics and Space Administration :, 1967), by Donald W. Petrasek, John W. Weeton, Robert A. Signorelli, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6140 (National Aeronautics and Space Administration ;, 1971), by L. David Wall, Michael F. Card, Langley Research Center, and United States National Aeronautics and Space Administration (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)
• Fiberglass reinforced polymer composite bridge deck construction in Illinois (Illinois Dept. of Transportation, Bureau of Materials and Physical Research ;, 2002), by Thomas J. Winkelman and Illinois. Dept. of Transportation. Bureau of Materials and Physical Research (page images at HathiTrust)
• Preparation and properties of fiber-reinforced structural materials (Columbus, Ohio : Battelle Memorial Institute, Defense Metals Information Center, 1963., 1963), by D. E. Price, H. J. Wagner, and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Fiber-reinforced metal-matrix composites : government sponsored research, 1964-1966 (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1967., 1967), by C. M. Jackson, H. J. Wagner, and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Fiber-reinforced metal-matrix composites--1967 (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1968., 1968), by K. R. Hanby and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Fiber-reinforced metal-matrix composites--1968 (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1969., 1969), by K. R. Hanby and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Fiber-reinforced metal-matrix composites--1969-1970 (Defense Metals Information Center, Battelle Memorial Institute, 1971), by K. R. Hanby and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Concrete tunnel liners : structural testing of cast-in-place liners : final report (Federal Railroad Administration, Dept. of Transportation ;, 1975), by S. L. Paul, R A Ferrera-Boza, University of Illinois at Urbana-Champaign. Dept. of Civil Engineering, and United States. Federal Railroad Administration (page images at HathiTrust)
• Microdynamics of wave propagation (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), by Alberto Puppo, Juan Haener, Ming-yuan Feng, Air Force Materials Laboratory (U.S.), and Whittaker Corporation (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)
• 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)
• Development of nondestructive test techniques for multidirectional fiber-reinforced resin matrix composites (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by John L. Cook, Air Force Materials Laboratory (U.S.), and McDonnell Douglas Astronautics Company-West (page images at HathiTrust)
• Development of nondestructive test techniques for multidirectional fiber-reinforced resin matrix composites (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by John L. Cook, Air Force Materials Laboratory (U.S.), and McDonnell Douglas Astronautics Company-West (page images at HathiTrust)
• Stability of filament wound cylinders under combined loading (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by A. Holston, D. A. Stang, A. Feldman, Air Force Flight Dynamics Laboratory (U.S.), and Martin Marietta Denver Aerospace (page images at HathiTrust)
• Effects of cure and sizing on fiber-matrix bond strength (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), by Piet W. Peters, George S. Springer, Air Force Wright Aeronautical Laboratories, and Stanford University. Department of Aeronautics and Astronautics (page images at HathiTrust)
• Composite wing design for aeroelastic requirements ([Wright-Patterson Air Force Base, Ohio] : [Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force] 1972., 1972), by L. A. McCullers, R. W. Lynch, Air Force Flight Dynamics Laboratory (U.S.), General Dynamics Corporation. Convair Division, United States. Air Force. Systems Command, and Ohio) Conference on Fibrous Composites in Flight Vehicle Design ([1st] : 1972 : Dayton (page images at HathiTrust)
• Application of optimality criterion to fiber-reinforced composites (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by N. S. Khot, V. A. Tischler, C. D. Johnson, V. B. Venkayya, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)

• Fiber composite analysis and design : composite materials and laminates. Volume I (Federal Aviation Administration, Office of Aviation Research ;, 1997), by Zvi Hashin, Materials Sciences Corporation, and United States. Office of Aviation Research (page images at HathiTrust)
• Methods of analysis and of reporting fiber composition of textile products (Washington, D.C. : United States Department of Commerce, National Bureau of Standards, 1943., 1943), by United States. National Bureau of Standards (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)

• ICAN (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986), by P. L. N. Murthy and C. C. Chamis (page images at HathiTrust)

• Failure analysis and mechanisms of failure of fibrous composite structures (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)
• Assessment of carbon fiber electrical effects : an industry/government briefing held at Langley Research Center, Hampton, Virginia, December 4-5, 1979. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

• Acoustic emission monitoring of low velocity impact damage in graphite/epoxy laminates during tensile loading (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Bradford H. Parker and Goddard Space Flight Center (page images at HathiTrust)

• Effect of low-speed impact damage and damage location on behavior of composite panels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Dawn C. Jegley and Langley Research Center (page images at HathiTrust)
• Acoustic emission monitoring of low velocity impact damage in graphite/epoxy laminates during tensile loading (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Bradford H. Parker and Goddard Space Flight Center (page images at HathiTrust)
• Fundamental mechanisms of tensile fracture in aluminum sheet unidirectionally reinforced with boron filament (National Aeronautics and Space Administration ;, 1972), by Harvey W. Herring and Langley Research Center (page images at HathiTrust)
• Tensile behavior of boron-filament-reinforced epoxy rings and belts (National Aeronautics and Space Administration ;, 1969), by Robert M. Baucom, United States National Aeronautics and Space Administration, and Langley Research Center (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)

More items available under broader and related terms at left.