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Buckling (Mechanics) -- Mathematical models

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• Buckling (Mechanics)
• Deformations (Mechanics) -- Mathematical models
• Plasticity -- Mathematical models
• Strains and stresses -- Mathematical models
• Structural failures -- Mathematical models
• Mathematical models

• Buckling (Mechanics) -- Computer simulation

• 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)
• Buckling and vibration analysis of a simply supported column with a piecewise constant cross section (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Mark S. Lake, Martin M. Mikulas, and Langley Research Center (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)
• 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)
• 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)
• A finite element procedure for nonlinear prebuckling and initial postbuckling analysis (National Aeronautics and Space Administration, 1972), by S. T. Mau and Richard H. Gallagher (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)
• Post-buckling behavior of cylindrical shells (National Aeronautics and Space Administration, 1964), by A. V. Pogorelov (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)

• 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)
• 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)
• 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)
• 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)

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

• A study of the effects of penetration framing on steel containment buckling capacity (Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission :, 1987), by William E. Baker, Thomas A. Butler, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology, and Los Alamos National Laboratory (page images at HathiTrust)
• The buckling of curved tension-field girders (National Advisory Commitee for Aeronautics, 1938), by G. Limpert and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• The twisting of thin-walled, stiffened circular cylinders (National Advisory Commitee for Aeronautics, 1938), by E. Schapitz and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• Coal mine floor heave in the Beckley coalbed, an analysis (Dept. of the Interior, Bureau of Mines, 1978), by James R. Aggson (page images at HathiTrust)
• Buckle in veneer (U.S. Dept. of Agriculture, Forest Service, 1970), by J. F. Lutz, University of Wisconsin, and Forest Products Laboratory (U.S.) (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)
• 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)
• Buckling of simply supported plywood plates under combined edgewise bending and compression (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1965), by John J. Zahn and Karl Romstad (page images at HathiTrust)
• Material buckling measurements on graphite-uranium systems at Hanford : a summary tabulation (U.S. Atomic Energy Commission, 1961), by D. E. Wood, Hanford Works, and Hanford Atomic Products Operation (page images at HathiTrust)
• Calculated critical parameters for slightly enriched uranium rods in light water (U.S. Atomic Energy Commission, 1961), by C. L. Brown, Hanford Works, and Hanford Atomic Products Operation (page images at HathiTrust)
• A semi-empirical method of estimating material bucklings for slightly enriched uranium-water lattices (U.S. Atomic Energy Commission, 1961), by C. L. Brown, Hanford Works, and Hanford Atomic Products Operation (page images at HathiTrust)
• Investigation on buckling of rigid joint structures. (Ithaca, N. Y., 1949), by Cornell University. Department of Structural Engineering and P. P. Bijlaard (page images at HathiTrust)
• Thermal buckling of solid wings. (Polytechnic Institute of Brooklyn, Dept. of Aeronatical Engineering and Applied Mechanics, 1957), by Josef Singer (page images at HathiTrust)
• Torsional creep buckling of open tubes having arbitrary cross-section. (School of Aeronautical Engineering, Purdue University, 1959), by George Lianis (page images at HathiTrust)
• Buckling of uniformly compressed steel plates in the strain-hardening range. (Fritz Engineering Laboratory, Dept. of Civil Engineering, Lehigh University, 1956), by Geerhard Haaijer (page images at HathiTrust)
• Cyclic creep buckling of integrally stiffened aluminum alloy panels (Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1958), by C. W. King and B. J. Nolan (page images at HathiTrust)
• On the buckling of circular cylindrical shells under external pressure (Columbia University, Dept. of Civil Engineering and Engineering Mechanics, 1962), by Anthony E. Armenàkas and George Herrmann (page images at HathiTrust)
• Buckling and postbuckling behavior of compression-loaded isotropic plates with cutouts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
• Structural efficiency studies of corrugated compression panels with curved caps and beaded webs (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Randall C. Davis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Michael P. Nemeth, Eric R. Johnson, Manuel Stein, and Langley Research Center (page images at HathiTrust)
• Effect of end-ring stiffness on buckling of pressure-loaded stiffed conical shells (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Randall C. Davis, Jerry G. Williams, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Manuel Stein, P. Daniel Sydow, Liviu Librescu, and Langley Research Center (page images at HathiTrust)
• A buckling analysis for rectangular orthotropic plates with centrally located cutouts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Michael P. Nemeth and Langley Research Center (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)
• Buckling and failure characteristics of graphite-polyimide shear panels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Mark J. Shuart, Jane A. Hagaman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
• Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by P. Daniel Sydow, Mark J. Shuart, and Langley Research Center (page images at HathiTrust)
• The effect of edge constraint on the buckling of sandwich and ring-stiffened 120 degree conical shells subjected to external pressure (National Aeronautics and Space Administration, 1967), by Gerald A. Cohen (page images at HathiTrust)
• Upper and lower bounds for the eigenvalues of vibrating beams with linearly varying axial load (National Aeronautics and Space Administration ;, 1966), by William Laird, Guy Fauconneau, University of Pittsburgh, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The influence of prebuckling deformation on the buckling load of truncated conical shells under axial compression (National Aeronautics and Space Administration, 1967), by Shigeo Kobayashi (page images at HathiTrust)
• Edge conditions (National Aeronautics and Space Administration, 1965), by B. O. Almroth, Lockheed Missiles and Space Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Buckling of imperfect cylinders under axial compression (National Aeronautics and Space Administration, 1966), by G. A. Thurston and M. A. Freeland (page images at HathiTrust)
• An experimental study of the buckling of complete spherical shells (National Aeronautics and Space Administration, 1966), by R. L. Carlson, N. J. Hoff, and R. L. Sendelbeck (page images at HathiTrust)
• Buckling of cylindrical shell end closures by internal pressure (National Aeronautics and Space Administration, 1966), by G. A. Thurston and A. A. Holston (page images at HathiTrust)
• The influence of the boundary conditions on the buckling load of cylindrical shells under axial compression (National Aeronautics and Space Administration, 1966), by Shigeo Kobayashi (page images at HathiTrust)
• Almost sure stability of long cylindrical shells with random imperfections (National Aeronautics and Space Administration, 1968), by Rena Scher Fersht (page images at HathiTrust)
• Buckling of conical shells under axial compression (National Aeronautics and Space Administration, 1968), by Johann Arbocz (page images at HathiTrust)
• Experimental investigation of the effect of general imperfections on the buckling of cylindrical shells (National Aeronautics and Space Administration]; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Johann Arbocz, Charles D. Babcock, and California Institute of Technology (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)
• Advanced beaded and tubular structural panels (National Aeronautics and Space Administration ;, 1975), by Max D. Musgrove, Bruce E. Greene, Langley Research Center, and Boeing Aerospace Company (page images at HathiTrust)
• DESAP 2 : a structural design program with stress and buckling constaints (National Aeronautics and Space Administration ;, 1977), by Jaan Kiusalaas, G. B. Reddy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A digital computer study of the buckling of shallow spherical caps and truncated hemispheres (National Aeronautics and Space Administration ;, 1972), by William C. Stilwell, Robert E. Ball, Langley Research Center, and Naval Postgraduate School (U.S.) (page images at HathiTrust)
• Feasibility study of shell buckling analysis using the modified structure method (National Aeronautics and Space Administration ;, 1972), by Gerald A. Cohen, Raphael T. Haftka, Langley Research Center, and Structures Research Associates (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)
• The buckling analysis of imperfection sensitive shell structures / Johann Arbocz and Charles D. Babcock, Jr. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Johann Arbocz, Charles D. Babcock, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• NASA TN D-2005 (National Aeronautics and Space Administration, 1963), by Charles D. Babcock, E. E. Sechler, California Institute of Technology, and United States National Aeronautics and Space Administration (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)
• Statistical methods in the nonlinear theory of elastic shells ... : Presented at a seminar in the Institute of Mechanics of the Academy of Sciences USSR on 3 October 1957 (National Aeronautics and Space Administration, 1962), by V. V. Bolotin (page images at HathiTrust)
• The effect of ring distortions on buckling of blunt conical shells (National Aeronautics and Space Administration ;, 1975), by Walter L. Heard, Wendell B. Stephens, Melvin S. Anderson, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6479 (National Aeronautics and Space Administration :, 1971), by Gary L. Giles, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5782 (National Aeronautics and Space Administration :, 1970), by Jerrell M. Thomas, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5980 (National Aeronautics and Space Administration :, 1970), by Sidney C. Dixon, John B. Carine, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5759 (National Aeronautics and Space Administration :, 1970), by Sidney C. Dixon, M. Latrelle Hudson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mechanical properties of advanced gravity gradient booms (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by C. L. Staugaitis and R. E. Predmore (page images at HathiTrust)
• Plastic buckling of plates and shells under biaxial loading (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by James P. Peterson (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)
• NASA TN D-5508 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Charles P. Shore, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3831 (National Aeronautics and Space Administration :, 1967), by Paul A. Cooper and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3089 (National Aeronautics and Space Administration ;, 1966), by John N. Dickson, Richard H. Brolliar, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4124 (National Aeronautics and Space Administration ;, 1967), by George E. Weeks and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mechanical properties and column behavior of thin-wall Be-38Al alloy tubing (National Aeronautics and Space Administration ;, 1969), by Donald R. Rummler and Langley Research Center (page images at HathiTrust)
• Buckling tests of two integrally stiffened cylinders subjected to bending (National Aeronautics and Space Administration ;, 1971), by James Kent Anderson, James P. Peterson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Buckling tests of two 4.6-meter-diameter, magnesium ring-stiffened conical shells loaded under external pressure (National Aeronautics and Space Administration ;, 1973), by James Kent Anderson, Randall C. Davis, United States National Aeronautics and Space Administration, and Langley Research Center (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)
• Buckling of light water lattices (.600" diameter rods, 1.3% and 1.15% 25) (United States Atomic Energy Commission, Technical Information Service, 1955), by Herbert J. Kouts, U.S. Atomic Energy Commission, and Brookhaven National Laboratory (page images at HathiTrust)
• Buckling of light-water moderated lattices of .387" diameter, 1.027% enriched uranium rods (United States Atomic Energy Commission, Technical Information Service, 1955), by Herbert J. Kouts, U.S. Atomic Energy Commission, and Brookhaven National Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1940), by Eugene E. Lundquist, Joseph N. Kotanchik, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• A model study for vertical track buckling (Federal Railroad Administration, Office of Research, Development and Demonstrations, 1971), by Arnold D. Kerr, New York University. Department of Aeronautics and Astronautics, United States. Office of High-Speed Ground Transportation, and Development United States. Federal Railroad Administration. Office of Research (page images at HathiTrust)
• Damage assessment and confinement in offshore pipelines (U.S. Department of Transportation, Research and Special Programs Administration ;, 1983), by S. Kyriakides, C. D. Babcock, United States. Department of Transportation. Office of University Research, and California Institute of Technology (page images at HathiTrust)
• Critical stress of ring-stiffened cylinders in torsion (National Advisory Committee for Aeronautics, 1949), by Manuel Stein, Harold Crate, J. Lyell Sanders, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Buckling of thin-walled cylinder under axial compression and internal pressure (National Advisory Committee for Aeronautics, 1950), by Hsu Lo, Edward B. Schwartz, Harold Crate, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lateral elastic instability of hat-section stringers under compressive load (National Advisory Committee for Aeronautics, 1951), by Stanley Goodman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Use of a variational principle in the numerical determination of the buckling eigenvalues of a thin rectangular plate (Union Carbide Nuclear Company, 1962), by Robert G. Edwards, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Study of instantaneous collapse and creep buckling characteristics of large sodium graphite reactor process tubes (Atomics International, 1965), by M. Lemcoe, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• A Numerical approach to the instability problem of monocoque cylinders (National Advisory Committee for Aeronautics, 1951), by Bruno A. Boley, Mayers. J., Josesph Kempner, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Extension of the safe geometric parameters to slightly enriched uranium (Union Carbide Nuclear Company, Oak Ridge Gaseous Diffusion Plant, 1958), by C. E. Newlon, H. F. Henry, Oak Ridge Gaseous Diffusion Plant, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The buckling of plates and shells. (Macmillan, 1963), by H. L. Cox (page images at HathiTrust)
• The effect of buckling on the multigroup diffusion theory group constants calculated by the MUFT code (Washington, D.C. : Office of Technical Services, Department of Commerce, 1957., 1957), by R. S. Wick, U.S. Atomic Energy Commission, Westinghouse Electric Corporation, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Snap-through and post-buckling behavior of cylindrical shells under the action of external pressure (Urbana, 1957), by Henry L. Langhaar and Arthur P. Boresi (page images at HathiTrust)
• Non-linear bending and buckling of circular plates (New York, New York : AEC Computing and Applied Mathematics Center, Institute of Mathematical Sciences, New York University, 1958., 1958), by Herbert Bishop Keller, Edward L. Reiss, New York University. Institute of Mathematical Sciences, and U.S. Atomic Energy Commission. New York Operations Office (page images at HathiTrust)
• Analytical investigation of buckling and post-buckling behavior of cylindrical shells (Dept. of Theoretical and Applied Mechanics, University of Illinois, 1957), by Henry L. Langhaar, Arthur P. Boresi, and University of Illinois (Urbana-Champaign campus). Department of Theoretical and Applied Mechanics (page images at HathiTrust)
• A Koiter-type method for finite element analysis of nonlinear structural behavior. Volume 2, User's manual for program BEHAVE (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by Raphael T. Haftka, W. Nachbar, R. H. Mallett, San Diego University of California, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Influence of residual stresses and thermal gradients on mechanism of buckling of shallow spherical shells (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 Megumi Sunakawa, R. M. Evan-Iwanowski, Air Force Flight Dynamics Laboratory (U.S.), and Syracuse University. Research Institute (page images at HathiTrust)
• Thermal buckling (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), by Frederick V. Pohle, Irwin Berman, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. |b Department of Aeronautical Engineering and Applied Mechanics (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)
• A technique for obtaining improved real-time holographic interferometric data using pulse modulated illumination (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Structural Analysis Group, Structures Division, Air Force Systems Command, United States Air Force, 1971., 1971), by Frank D. Adams, Gene E. Maddux, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Investigation of the creep buckling behavior of columns : Part I Elevated temperature properties of the test material Ti-7AI-4Mo Titanium Alloy (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Ralph Papirno, George Gerard, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and New York University (page images at HathiTrust)
• Dynamic buckling of shell structures subject to longitudinal impact (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by A. P. Coppa, W. A. Nash, United States. Air Force. Systems Command. Aeronautical Systems Division, and General Electric Company (page images at HathiTrust)
• General instability of orthotropically stiffened cylinders. Part 2, Bending and combined compression and bending (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, AIr Force Systems Command, United States Air Force, 1965., 1965), by C. Lakshmikantham, Roger Milligan, George Gerard, Allied Research Associates, and Air Force Flight Dynamics Laboratory (U.S.) (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)
• Flexible plates and shells; a translation of [Gibkie plastinki i obolochki] (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. S. Volʹmir, Air Force Flight Dynamics Laboratory (U.S.), and University of Florida. Department of Engineering Sciences (page images at HathiTrust)
• Experimental and numerical analysis of axially compressed circular cylindrical fiber-reinforced panels with various boundary conditions (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 Nelson R. Bauld, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Clemson University. Department of Mechanical Engineering (page images at HathiTrust)
• Investigation of the creep buckling behavior of columns: Part II Creep buckling experiments with columns of Ti-7AI-4Mo Titanium alloy (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), by Ralph Pairno, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and New York University (page images at HathiTrust)
• A Koiter-type method for finite element analysis of nonlinear structural behavior. Volume 1, The Modified Structure method (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by Raphael T. Haftka, W. Nachbar, R. H. Mallett, San Diego University of California, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• An investigation of the creep buckling behavior of columns : Part V Theory of creep buckling of perfect plates and shells (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1962., 1962), by George Gerard, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and New York University (page images at HathiTrust)
• Buckling of composites under hot and wet environment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), by V. Sarma Avva, L. Sharpe, D. Yogi Goswami, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and North Carolina Agricultural and Technical State University (page images at HathiTrust)
• Correlation of plate creep buckling theory with experiments on long plates of aluminum alloy 2024-0 at 500° F (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Ralph Papirno, George Gerard, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and New York University (page images at HathiTrust)
• General instability of orthotropically stiffened cylinders. Part 1, Axial compression, torsion and hydrostatic pressure loadings (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, AIr Force Systems Command, United States Air Force, 1965., 1965), by Roger Milligan, Herbert Becker, C. Lakshmikantham, George Gerard, Allied Research Associates, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• An investigation of column action during creep buckling (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by R. L. Carlson, G. K. Manning, W. W. Breindel, Aerospace Research Laboratories (U.S.), United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and Battelle Memorial Institute (page images at HathiTrust)
• Collapse analysis for shells of general shape. Volume 1, Analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by Bo O. Almroth, M. B. Marlowe, F. A. Brogan, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed Palo Alto Research Laboratory (page images at HathiTrust)
• Development of experimental testing programs to verify thermal stress analysis (Wright-Patterson AIr Force Base, Ohio : Air Force Flight Dynamicas Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by B. E. Gatewood, B. H. Ulrich, A. R. Glaser, Ohio State University. Department of Aeronautical and Astronautical Engineering, and Air Force Flight Dynamics Laboratory (U.S.) (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)
• Collapse analysis for shells of general shape. Volume 2. User's manual for the STAG-A computer code (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Bo O. Almroth, H. T. Petersen, F. Zele, E. Meller, F. A. Brogan, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed Palo Alto Research Laboratory (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)
• BUCKDEL v 0.9 users and theory manuals : buckling and delamination analysis of stiffened laminated plates (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Materiel Command, United States Air Force, 1996., 1996), by Daniel S. Pipkins, Satya N. Atluri, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (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)
• 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)
• Implementation of a damage tolerance module into ASTROS (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Materiel Command, United States Air Force, 1996., 1996), by Daniel S. Pipkins, Satya N. Atluri, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Numerical methods for imperfection sensitivity analysis of stiffened cylindrical shells. Volume 1. Development and applications (Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986), by Richard L. Citerley, Narendra S. Khot, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)

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