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Laminated materials -- Thermal properties

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• Laminated materials
• Composite materials -- Thermal properties
• Plates (Engineering) -- Thermal properties
• Thermal properties

• Laminated plastics -- Thermal properties
• Sandwich construction -- Thermal properties

• Analysis of thermal degradation of glass reinforced phenolic and epoxy laminates (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Harry S. Wilson, J. E. Katon, Ival O. Salyer, Dayton Laboratory, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Transient heat flow along uni-directional 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, 1982., 1982), by Lit S. Han, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Ohio State University. Research Foundation (page images at HathiTrust)

• Investigation of thermal properties of plastic laminates, cores, and sandwich panels (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955, 1955), by F. R. O'Brien, S. Oglesby, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)

• Investigation of thermal properties of plastic laminates, cores, and sandwich panels (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955, 1955), by F. R. O'Brien, S. Oglesby, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)

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

• Development of a test method to evaluate the penetration resistance of high-security glazing subjected to mechanical impact and heat (U.S. Dept. of Justice, National Institute of Justice, 1986), by Lawrence I. Knab and National Institute of Justice (U.S.) (page images at HathiTrust)
• Three-dimensional analysis of a postbuckled embedded delamination (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by J. D. Whitcomb and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Trends in international trade in printed circuit boards and base material laminates report to the Subcommittee on Trade of the Committee on Ways and Means of the U.S. House of Representatives on investigation no. 332-133 under section 332 of the Tariff Act of 1930. (U.S. International Trade Commission, 1983), by United States International Trade Commission, Nelson Hogge, and United States. Congress. House. Committee on Ways and Means (page images at HathiTrust)
• Impact tests on fibrous composite sandwich structures (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Marvin D. Rhodes, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Fracture toughness of boron/aluminum laminates with various proportions of 0° and ±45 ̊plies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by C. C. Poe, J. A. Sova, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• A new look at numerical analyses of free-edge stresses in composite laminates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by I. S. Raju, J. G. Goree, J. D. Whitcomb, Langley Research Center, Joint Institute for Advancement of Flight Sciences, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An improved transverse shear deformation theory for laminated anisotropic plates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by M. V. V. Murthy, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• 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)
• An experimental feasibility study for the preparation of thermo-oxidatively stable Pyrrone laminates (National Aeronautics and Space Administration ;, 1969), by H. R. Lubowitz, Langley Research Center, and TRW Systems Group (page images at HathiTrust)
• Preliminary investigation of crack arrest in composite laminates containing buffer strips (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by J. G. Goree and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (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)
• Fracture behavior of thick, laminated graphite/epoxy composites (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Charles E. Harris, D. H. Morris, Virginia Polytechnic Institute and State University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Tensile stress-strain behavior of graphite/epoxy laminates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by D. P. Garber, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Kentron Technical Center, and Langley Research Center (page images at HathiTrust)
• Repair techniques for Celion/LARC-160 graphite/polyimide composite structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by J. S. Jones, Rockwell International, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center, and S.R. Graves (page images at HathiTrust)
• Development of tough, moisture resistant laminating resins (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by R. A. Brand, E. S. Harrison, General Dynamics Corporation. Convair Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Analysis of laminated, composite, circular cylindrical shells with general boundary conditions (National Aeronautics and Space Administration, 1974), by S. Srinivas and Langley Research Center (page images at HathiTrust)
• NASA TN D-3918 (National Aeronautics and Space Administration ;, 1967), by John G. Davis, George W. Zender, 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)
• Feasibility study on the development of tough, moisture-resistant laminating resins (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by R. A. Brand, E. S. Harrison, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Strength of heat-resistant laminates up to 375©� C (National Advisory Committee for Aeronautics, 1951), by B. M. Axilrod, Martha A. Sherman, and United States. National Advisory Committee for Aeronautics (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)
• 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)
• 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)
• 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)
• 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)
• Metal-ceramic laminates (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by R Francis, J. R. Tinklepaugh, E. P. McNamara, R. Brown, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and State University of New York 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 (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)

• 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)

• 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)

• Tough composite materials (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)

• An optimal design of simple symmetric laminates under the first ply failure criteria (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Won J. Park, Air Force Wright Aeronautical Laboratories, and Inc Universal Energy Systems (page images at HathiTrust)

• Effect of electron irradiation on some properties of the Echo II laminate (National Aeronautics and Space Administration :, 1964), by Thomas G. James and Langley Research Center (page images at HathiTrust)

• Evaluation of a hybrid anisotropic, multilayered, quadrilateral finite element (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by James Campbell Robinson, Charles L. Blackburn, University of Tennessee at Nashville, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

• Nonlinear effects on composite laminate thermal expansion (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Z. Hashin, R. Byron Pipes, B. W. Rosen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

• Die Familie Vanderhouten (Morawe & Scheffelt, 1917), by Adele Gerhard (page images at HathiTrust; US access only)

• 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)

• Instructions for TI-59 combined card/module calculations for in-plane properties of symmetric hybrid laminates (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Stella D. Gates and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• The effects of thermal spiking on graphite-epoxy composites (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1979., 1979), by George S. Springer, A. C. Loos, Air Force Materials Laboratory (U.S.), and University of Michigan. Department of Mechanical Engineering (page images at HathiTrust)
• On design of off-axis specimens (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 Raghbir Singh Sandhu, George Peter Sendeckyj, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Inc Analytical Methods (page images at HathiTrust)
• Revised instructions for TI-59 combined card/module calculations for in-plane and flexural properties of symmetric laminates (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Steven L. Donaldson and Air Force Wright Aeronautical Laboratories (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)

More items available under broader and related terms at left.