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Sandwich construction

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• Laminated materials
• Lightweight construction

• Sandwich construction -- Bibliography
• Sandwich construction -- Elastic properties
• Sandwich construction -- Materials
• Sandwich construction -- Mathematical models
• Sandwich construction -- Mechanical properties
• Sandwich construction -- Testing
• Sandwich construction -- Thermal properties
• Sandwich construction -- Vibration
• Honeycomb structures

• Sandwich construction for aircraft; ANC-23 bulletin. (Dep. of the Air Force, Air Research and Development Command, 1955), by Forest Products Laboratory (U.S.) and United States. ANC-23 Panel on Sandwich Construction for Aircraft (page images at HathiTrust)
• Paper honeycomb sandwich panels as lightweight structural components (National Bureau of Standards; for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1972), by T. W. Reichard (page images at HathiTrust)
• Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression (1956), by William R. Kimel (page images at HathiTrust; US access only)
• Compressive and shear properties of polyamide honeycomb core (U.S. Dept. of Agriculture, Forest Service, 1974), by Edward W. Kuenzi, Paul M. Jenkinson, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Bending of a circular sandwich plate by load applied through an insert (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1973), by Henry M. Montrey (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)
• Optimum distribution of material in sandwich plates loaded in their plane. Including plates with varying modulus of elasticity. (Cornell Aeronautical Laboratory, Inc., 1950), by P. P. Bijlaard (page images at HathiTrust)
• Composite construction for flight vehicles. (Armed Forces Supply Support Center, 1959), by United States. Dept. of Defense (page images at HathiTrust)
• Sandwich construction for aircraft. (Subcommittee on Air Force-Navy-Civil Aircraft Design Criteria, Munitions Board Aircraft Committee, 1951), by Forest Products Laboratory (U.S.) and United States. Munitions Board. Aircraft Committee. Subcommittee on Air Force-Navy-Civil Aircraft Design Criteria (page images at HathiTrust)
• Sandwich construction for aircraft : ANC-23 bulletin (Dept. of the Air Force, Air Research and Development Command, 1955), by Forest Products Laboratory (U.S.) and United States. ANC-23 Panel on Sandwich Construction for Aircraft (page images at HathiTrust)
• Elastic instability of rectangular sandwich panel of orthotropic core with different face thicknesses and materials (Institute of Technology, University of Minn.], 1958), by Chieh C. Chang and Ibrahim K. Ebcioglu (page images at HathiTrust)
• Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
• Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
• In the matter of certain molded-in sandwich panel inserts and methods for their installation : investigation no. 337-TA-99 (modification proceeding). (U.S. International Trade Commission, 1982), by United States International Trade Commission (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)
• 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)
• 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)
• Tests of graphite/polymide sandwich panels in uniaxial edgewise compression (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1980), by Charles J. Camarda, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Mechanical property characterization of Borsic®/aluminum laminates at room and elevated temperatures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Robert R. McWithey, Dick M. Royster, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Structural optimization of sandwich and ring-stiffened 120 degree conical shells subjected to external pressure (National Aeronautics and Space Administration ;, 1969), by Gerald A. Cohen, Langley Research Center, and Philco-Ford Corporation (page images at HathiTrust)
• Design data for brazed Rene ́41 honeycomb sandwich (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Andrew K. Hepler, Boeing Aerospace Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Buckling tests of three 4.6 meter diameter aluminum honeycomb sandwich conical shells loaded under external pressure (National Aeronautics and Space Administration ;, 1975), by James Kent Anderson, Randall C. Davis, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6427 (National Aeronautics and Space Administration ;, 1971), by Larry L. Erickson, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-2783 (National Aeronautics and Space Administration :, 1965), by Robert E. Fulton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Small bending and stretching of sandwich-type shells (National Advisory Committee for Aeronautics, 1949), by Eric Reissner and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Properties of honeycomb cores as affected by fiber type, fiber orientation, resin type, and amount (National Advisory Committee for Aeronautics, 1951), by R. J. Seidl, A. W. Voss, D. J. Fahey, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Elevated-temperature tests under static and aerodynamic conditions on honeycomb-core sandwich panels (National Aeronautics and Space Administration, 1959), by Joseph M. Groen, Aldie E. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of brazed honeycomb structures (Ohio State University Research Foundation, 1960), by Ohio State University. Department of Welding Engineering and Robert Charles McMaster (page images at HathiTrust)
• Building with plastic structural sandwich panels (Monsanto Chemical Co., Plastics Division, 1958), by Bernard P. Spring, Lawrence B. Anderson, and Massachusetts Institute of Technology. Dept. of Agriculture (page images at HathiTrust)
• Structural sandwich construction (United States Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1952), by University of Wisconsin and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Paper-honeycomb cores for structural sandwich panels (United States Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1952), by R. J. Seidl, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Results of some tests on low-density materials (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1944), by E. C. O. Erickson, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Application of composite constructions with honeycomb and foam cores (Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1961), by Wendell T. Jackson, United States. Air Force. Air Research and Development Command, Wright Air Development Division, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• The damping of aluminum honeycomb sandwich beams (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by D. J. Mead, G. R. Froud, United States. Air Force. Systems Command. Aeronautical Systems Division, and University of Southampton (page images at HathiTrust)
• Optimality criteria in structural design (Wright-Patterson Air Force Base, Ohio : Air Force Systems Command, Air Force Flight Dynamics Laboratory, United States Air Force, 1971., 1971), by William Prager, Pedro V. Marcal, Air Force Flight Dynamics Laboratory (U.S.), and Brown University. Division of Engineering (page images at HathiTrust)
• Preliminary design of wings. Volume IV, Minimum weight design of composite structure (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Harold Switzky, Air Force Flight Dynamics Laboratory (U.S.), and Fairchild Republic Company (page images at HathiTrust)
• Development of brazed sandwich construction materials for high temperature applications (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Charles F. Burrows, F. J. Ragland, United States. Air Force. Air Research and Development Command, Martin Company, and Wright Air Development Center (page images at HathiTrust)
• Thermo-elastic equations for a sandwich panel under arbitrary temperature distribution, transverse load and edge compression (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Ibrahim K. Ebcioglu, United States. Air Force. Systems Command. Aeronautical Systems Division, and United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States (page images at HathiTrust)
• Matrix analysis of shells : small and large displacements (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), by J. H. Argyris, P. C. Patton, K. E. Buck, W. Bosshard, J. B. Spooner, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• The analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by Thomas N. Bernstein, Robert M. Engle, Gene E. Maddux, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• The minimum weight design of structures operating in an aerospace environment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by H. Switzky, United States. Air Force. Systems Command. Aeronautical Systems Division, and Republic Aviation Corporation (page images at HathiTrust)

• For the space age; a bibliography of sandwich plates and shells ([Santa Monica, Calif.], 1962), by inc. Missile & Space Systems Division Douglas Aircraft Company and J. I. Foss (page images at HathiTrust)

• Experimental confirmation of thermo-elastic equations for sandwich panel deflection (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by I. K. Ebcioglu, K. D. Shimmin, J. R. Schmermund, J. A. Roberson, United States. Air Force. Systems Command. Aeronautical Systems Division, and Air Force Materials Laboratory (U.S.) (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)

• Fire endurance under design load for walls of one-story, three-room structures of sandwich and wood-frame construction (Forest Products Laboratory, Forest Service, U.S. Dept. of Agriculture, 1980), by Herbert W. Eickner, United States Department of Housing and Urban Development, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Fatigue properties of titanium and nickel-base sandwich constructions (Forest Products Laboratory, Forest Service, U.S. Dept. of Agriculture, 1970), by Paul M. Jenkinson (page images at HathiTrust)
• Edgewise compressive and fatigue properties of brazed titanium sandwich constructions (Forest Products Laboratory, Forest Service, U.S. Dept. of Agriculture, 1973), by G. H. Stevens (page images at HathiTrust)
• Mechanical properties of diffusion-bonded titanium sandwich constructions (Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1973), by Edward W. Kuenzi and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Structural evaluation of steel faced sandwich panels (National Bureau of Standards, [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1974), by J. H. Pielert, Larry W. Masters, T. W. Reichard, Center for Building Technology, United States. National Bureau of Standards, and United States Department of Housing and Urban Development Office of Policy Development and Research (page images at HathiTrust)
• Aluminum facing and aluminum honeycomb core sandwich material tested in shear (USDA, Forest Service, Forest Products Laboratory, 1949), by Fred Werren, University of Wisconsin, and Forest Products Laboratory (U.S.) (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)

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