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Elastic plates and shells -- Mathematical models

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• Elastic plates and shells
• Elasticity -- Mathematical models
• Plasticity -- Mathematical models
• Elastic plates and shells -- Simulation methods
• Mathematical models

• Elastic plates and shells -- Computer simulation
• Plates (Engineering) -- Mathematical models
• Shells (Engineering) -- Mathematical models
• Elastic plates and shells -- Simulation methods -- Mathematical models
• Elastic plates and shells -- Vibration -- Mathematical models

• Modal interaction in postbuckled plates : theory (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Gaylen A. Thurston and Langley Research Center (page images at HathiTrust)
• Application of Newton's method to postbuckling of rings under pressure loadings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Gaylen A. Thurston 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)
• Theoretical study of corrugated plates : shearing of a trapezoidally corrugated plate with through lines permitted to curve (National Aeronautics and Space Administration, 1971), by Chuan-jui Lin, Charles Libove, United States. National Aeronautical and Space Administration, Syracuse University, and Langley Research Center (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)
• 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)
• Shearing of a corrugated plate with curvilinear corrugations (National Aeronautics and Space Administration ;, 1972), by Lung-Hsiang Wu, Charles Libove, Langley Research Center, and Syracuse University (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)
• New triangular and quadrilateral plate-bending finite elements (National Aeronautics and Space Administration ;, 1974), by R. Narayanaswami and Langley Research Center (page images at HathiTrust)
• Multi-ring plates : a Step function approach ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], [1958], 1958), by Patrick M. Quinlan, United States. Air Force. Office of Scientific Research, and National University of Ireland (page images at HathiTrust)

• Mixed formulation for frictionless contact problems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Ahmed Khairy Noor and Kyun O. Kim (page images at HathiTrust)
• The effect of angle of attack on the buckling of Mars entry aeroshells (National Aeronautics and Space Administration ;, 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)

• Structural performance of two aerobrake hexagonal heat shield panel concepts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Dorsey, James W. Dyess, and Langley Research Center (page images at HathiTrust)
• Stress concentrations for straight-shank and countersunk holes in plates subjected to tension, bending, and pin loading (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by K. N. Shivakumar, J. C. Newman, and Langley Research Center (page images at HathiTrust)
• An elastoplastic analysis of a uniaxially loaded sheet with an interference-fit bolt (National Aeronautics and Space Administration ;, 1974), by John H. Crews and Langley Research Center (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)

• Turbulent fluid friction of rotating disks (National Aeronautics and Space Administration ;, 1973), by P. Cooper, Lewis Research Center, and Case Western Reserve University (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)

• Continuous skewed slabs (Engineering Experiment Station, College of Engineering, Ohio State University, 1959), by Asim Yeginobali (page images at HathiTrust)

• An analytical determination of temperature oscillations in a wall heated by alternating current (National Aeronautics and Space Administration, 1962), by Frank A. Jeglic and Lewis Research Center (page images at HathiTrust)

• Buckling of conical shell with local imperfections (National Aeronautics and Space Administration ;, 1974), by Paul A. Cooper, Cornelia B. Dexter, and Langley Research Center (page images at HathiTrust)
• Transient response of shells of revolution by direct integration and modal superposition methods (National Aeronautics and Space Administration ;, 1974), by Wendell B. Stephens, Howard M. Adelman, and Langley Research Center (page images at HathiTrust)
• Computer analysis of multicircuit shells of revolution by the field method (National Aeronautics and Space Administration ;, 1975), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)

• An analytical determination of temperature oscillations in a wall heated by alternating current (National Aeronautics and Space Administration, 1962), by Frank A. Jeglic and Lewis Research Center (page images at HathiTrust)

• Free vibrations of thermally stressed orthotropic plates with various boundary conditions (National Aeronautics and Space Administration ;, 1973), by C. D. Bailey, James C. Greetham, Langley Research Center, and Ohio State University. Research Foundation (page images at HathiTrust)

• Stress analysis of reinforced circular and rectangular flat plates (Argonne National Laboratory, 1965), by J. L. S. Chen, Donald A. Moen, and Chia-shing Lai (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)
• Compressive buckling analysis of hat-stiffened panel (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)
• A solution procedure for behavior of thick plates on a nonlinear foundation and postbuckling behavior of long plates (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Manuel Stein, Peter A. Stein, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Dissociative relaxation of oxygen over an adiabatic flat plate at hypersonic Mach numbers (National Aeronautics and Space Administration, 1960), by Paul M. Chung, Aemer D. Anderson, and Ames Research Center (page images at HathiTrust)
• BAFL-1 : a program for the solution of thin elastic plate equations on the PHILCO-2000 computer (Washington, D.C. : Office of Technical Services, Department of Commerce, 1961., 1961), by J. B. Callaghan, A. K. Rigler, P. H. Jarvis, Westinghouse Electric Corporation, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Preliminary design of wings. Volume III, Minimum weight design of stiffened plate (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)
• 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)

• Analysis of laminar flow between stationary and rotating disks with inflow (National Aeronautics and Space Administration ;, 1974), by Upendra S. Rohatgi, Eli Reshotko, Lewis Research Center, and Case Western Reserve University (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)

• Analysis of turbulent flow and heat transfer on a flat plate at high mach numbers with variable fluid properties (U.S. G.P.O.], 1959), by R. G. Deissler (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)

• On Reissner's theory of the bending of plates (National Aeronautics and Space Administration, 1960), by A. L. Golʹdenveĭzer (page images at HathiTrust)

• Analysis of turbulent flow and heat transfer on a flat plate at high mach numbers with variable fluid properties (U.S. G.P.O.], 1959), by R. G. Deissler (page images at HathiTrust)
• Nonlinear heat transfer and temperature distribution through fins and electric filaments of arbitrary geometry with temperature-dependent properties and heat generation (National Aeronautics and Space Administration ;, 1968), by Ahmad Raafat Shouman and George C. Marshall Space Flight Center (page images at HathiTrust)
• A three-dimensional analysis of the effects of heat generation in plates (National Aeronautics and Space Administration ;, 1968), by Robert R. McWithey and Langley Research Center (page images at HathiTrust)

• A triangular thin shell finite element : linear analysis (National Aeronautics and Space Administration ;, 1975), by G. R. Thomas, Richard H. Gallagher, Langley Research Center, and Cornell University (page images at HathiTrust)
• A triangular thin shell finite element : nonlinear analysis (National Aeronautics and Space Administration ;, 1975), by G. R. Thomas, Richard H. Gallagher, Langley Research Center, and Cornell University (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachment. Part VII, Work charts for off-center loading (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by M. T. Roche, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)

• Seal-shell : a digital program to determine stresses and deflections in an axisymmetric shell of revolution (Washington, D.C. : Office of Technical Services, Department of Commerce, 1961., 1961), by C. M. Friedrich, Westinghouse Electric Corporation, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)

• Applications of the theory of optimal control of distributed-parameter systems to structural optimization (National Aeronautics and Space Administration ;, 1972), by Jean-Louis Pierre Armand, Langley Research Center, and Stanford University (page images at HathiTrust)

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