The Online Books Page

Buckling (Mechanics)

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

• Deformations (Mechanics)
• Plasticity
• Strains and stresses
• Structural failures

• Buckling coefficients for sandwich cylinders of finite length under uniform external lateral pressure / (Madison, Wis. : 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 / (Madison, Wis. : U.S. Forest Products Laboratory, 1973), by John J. Zahn and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Buckle in veneer / (Madison, Wis. : 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 of simply supported plywood plates under combined edgewise bending and compression / (Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, [1965]), by John J. Zahn and Karl Romstad (page images at HathiTrust)
• The effect of initial displacement of the center support on the buckling of a column continuous over three supports / (Langley Field, VA : 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)
• The effect of ring distortions on buckling of blunt conical shells / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Walter L. Heard, Wendell B. Stephens, Melvin S. Anderson, and Langley Research Center (page images at HathiTrust)
• Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Jerrold M. Housner, Manuel Stein, and Langley Research Center (page images at HathiTrust)
• Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments / (Washington, D.C. : 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)
• Application of Newton's method to postbuckling of rings under pressure loadings / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Gaylen A. Thurston and Langley Research Center (page images at HathiTrust)
• Development of lightweight aluminum compression panels reinforced by boron-epoxy infiltrated extrusions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Paul A. Roy, Jim Henshaw, John A. McElman, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Buckling and postbuckling behavior of square compression-loaded graphite-expoxy plates with circular cutouts / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
• Evaluation of a metal shear web selectively reinforced with filamentary composites for space shuttle application / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by J. H. Laakso, J. W. Straayer, Langley Research Center, and Boeing Aerospace Company (page images at HathiTrust)
• Feasibility study of shell buckling analysis using the modified structure method / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Gerald A. Cohen, Raphael T. Haftka, Langley Research Center, and Structures Research Associates (page images at HathiTrust)
• Buckling and postbuckling behavior of compression-loaded isotropic plates with cutouts / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
• Buckling and vibration analysis of a simply supported column with a piecewise constant cross section / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Mark S. Lake, Martin M. Mikulas, and Langley Research Center (page images at HathiTrust)
• Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by A. V. Viswanathan, L. L. Baker, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by A. V. Viswanathan, R. E. Miller, Tsai-Chen Soong, Langley Research Center, and Boeing Company (page images at HathiTrust)
• Upper and lower bounds for the eigenvalues of vibrating beams with linearly varying axial load / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by William Laird, Guy Fauconneau, University of Pittsburgh, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of angle of attack on the buckling of Mars entry aeroshells / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)
• Buckling tests of two integrally stiffened cylinders subjected to bending / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), 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 (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by James Kent Anderson, Randall C. Davis, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Influence of edge conditions on the stability of axially compressed cylindrical shells / ([Washington] : 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)
• Minimum-weight designs for hat-stiffened composite panels under uniaxial compression / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Banarsi Agarwal, Randall C. Davis, and Langley Research Center (page images at HathiTrust)
• Investigation on buckling of rigid joint structures. (Ithaca, N. Y., 1949), by Cornell University. Dept. of Structural Engineering and P. P. Bijlaard (page images at HathiTrust)
• Modal interaction in postbuckled plates : theory / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Gaylen A. Thurston 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by James Kent Anderson, Randall C. Davis, and Langley Research Center (page images at HathiTrust)
• Torsional creep buckling of open tubes having arbitrary cross-section. (Lafayette, Ind., 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. (Bethlehem, Pa., Fritz Engineering Laboratory, Dept. of Civil Engineering, Lehigh University, 1956), by Geerhard Haaijer (page images at HathiTrust)
• Thermal buckling of solid wings. ([Brooklyn] Polytechnic Institute of Brooklyn, Dept. of Aeronatical Engineering and Applied Mechanics, 1957), by Josef Singer (page images at HathiTrust)
• Cyclic creep buckling of integrally stiffened aluminum alloy panels (Wright-Patterson Air Force Base, Ohio, 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, (New York, Columbia University, Dept. of Civil Engineering and Engineering Mechanics, 1962), by Anthony E. Armenàkas and George Herrmann (page images at HathiTrust)
• Preliminary design procedure for end rings of isotropic conical shells loaded by external pressure / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Sidney C. Dixon, John B. Carine, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Compressive instability and strength of uniaxial filament-reinforced epoxy tubes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by John G. Davis, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Vibration and buckling of prestressed shells of revolution / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1967), by Paul A. Cooper and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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 / (Washington : National Aeronautics and Space Administration, 1962), by V. V. Bolotin (page images at HathiTrust; US access only)
• Flutter, vibration, and buckling of truncated orthotropic conical shells with generalized elastic edge restraint / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Sidney C. Dixon, M. Latrelle Hudson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Mechanical properties of advanced gravity gradient booms, (Washington, 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; US access only)
• Thermal buckling analysis for stiffened orthotropic cylindrical shells / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by L. K. Chang (page images at HathiTrust; US access only)
• Buckling loads of stiffened panels subjected to combined longitudinal compression and shear : results obtained with PASCO, EAL, and STAGS computer programs / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by W. Jefferson Stroud, Melvin S. Anderson, William H. Greene, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Michael P. Nemeth, Eric R. Johnson, Manuel Stein, and Langley Research Center (page images at HathiTrust)
• Buckling of conical shell with local imperfections / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Paul A. Cooper, Cornelia B. Dexter, and Langley Research Center (page images at HathiTrust)
• Buckling behavior of long symmetrically laminated plates subjected to combined loadings / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
• Effect of end-ring stiffness on buckling of pressure-loaded stiffed conical shells / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• A buckling analysis for rectangular orthotropic plates with centrally located cutouts / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service,, 1984), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust)
• Tests of graphite/polymide sandwich panels in uniaxial edgewise compression / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
• Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compression / (Washington, D.C. : 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)
• Advanced beaded and tubular structural panels / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Jaan Kiusalaas, G. B. Reddy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A finite element procedure for nonlinear prebuckling and initial postbuckling analysis / (Washington, D.C. : National Aeronautics and Space Administration, [1972]), by S. T. Mau and Richard H. Gallagher (page images at HathiTrust)
• Structural efficiencies of five compression panels with curved elements / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Gary L. Giles, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Buckling of a pressurized toroidal ring under uniform external loading / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by George E. Weeks and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Structural efficiency studies of corrugated compression panels with curved caps and beaded webs / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Randall C. Davis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust)
• Stress analysis and buckling of J-stiffened graphite-epoxy panel. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Randall C. Davis, Langley Research Center, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Manuel Stein, P. Daniel Sydow, Liviu Librescu, and Langley Research Center (page images at HathiTrust)
• A digital computer study of the buckling of shallow spherical caps and truncated hemispheres / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by William C. Stilwell, Robert E. Ball, Langley Research Center, and Naval Postgraduate School (U.S.) (page images at HathiTrust)
• Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by A. V. Viswanathan, M. Tamekuni, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• The buckling analysis of imperfection sensitive shell structures / Johann Arbocz and Charles D. Babcock, Jr. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
• Post-buckling behavior of cylindrical shells / (Washington, D.C. : National Aeronautics and Space Administration, [1964]), by A. V. Pogorelov (page images at HathiTrust)
• A finite element approach to the structural instability of beam columns, frames, and arches / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Jerrell M. Thomas, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Minimum-mass design of filamentary composite panels under combined loads : design procedure based on a rigorous buckling analysis / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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-mass design of filamentary composite panels under combined loads : design procedure based on simplified buckling equations / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by W. Jefferson Stroud, Nancy Agranoff, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mechanical properties and column behavior of thin-wall Be-38Al alloy tubing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Donald R. Rummler and Langley Research Center (page images at HathiTrust)
• Plastic buckling of plates and shells under biaxial loading, ([Washington] 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; US access only)
• Experimental investigation of flutter at Mach 3 of rotationally restrained panels and comparison with theory / (Washington, D.C. : 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; US access only)
• The general instability of ring-stiffened corrugated cylinders under axial compression / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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; US access only)
• Effect of face-sheet stiffness on buckling of curved plates and cylindrical shells of sandwich construction on axial compression / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1965), by Robert E. Fulton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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; US access only)
• The effect of edge constraint on the buckling of sandwich and ring-stiffened 120 degree conical shells subjected to external pressure / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Gerald A. Cohen (page images at HathiTrust; US access only)
• The influence of prebuckling deformation on the buckling load of truncated conical shells under axial compression / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Shigeo Kobayashi (page images at HathiTrust; US access only)
• Buckling of imperfect cylinders under axial compression / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by G. A. Thurston and M. A. Freeland (page images at HathiTrust; US access only)
• An experimental study of the buckling of complete spherical shells / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by R. L. Carlson, N. J. Hoff, and R. L. Sendelbeck (page images at HathiTrust; US access only)
• Buckling of cylindrical shell end closures by internal pressure / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by G. A. Thurston and A. A. Holston (page images at HathiTrust; US access only)
• The influence of the boundary conditions on the buckling load of cylindrical shells under axial compression / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Shigeo Kobayashi (page images at HathiTrust; US access only)
• Almost sure stability of long cylindrical shells with random imperfections / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Rena Scher Fersht (page images at HathiTrust; US access only)
• Buckling of conical shells under axial compression / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Johann Arbocz (page images at HathiTrust; US access only)
• Experimental investigation of the effect of general imperfections on the buckling of cylindrical shells, ([Washington, 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; US access only)
• Damage assessment and confinement in offshore pipelines / (Washington, D.C. : U.S. Department of Transportation, Research and Special Programs Administration ; Springfield, Va. : National Technical Information Service [distributor], 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)
• A model study for vertical track buckling / (Washington, D.C. : 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)
• The twisting of thin-walled, stiffened circular cylinders / (Washington, D.C. : National Advisory Commitee for Aeronautics, [1938]), by E. Schapitz and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• Non-linear bending and buckling of circular plates /, 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)
• Critical stress of ring-stiffened cylinders in torsion / (Washington, D.C. : 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)
• Lateral elastic instability of hat-section stringers under compressive load / (Washington, D.C. : 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 / (Oak Ridge, Tenn. : Union Carbide Nuclear Company, 1962), by Robert G. Edwards, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Coal mine floor heave in the Beckley coalbed, an analysis / ([Washington, D.C.] : Dept. of the Interior, Bureau of Mines, [1978]), by James R. Aggson (page images at HathiTrust)
• Material buckling measurements on graphite-uranium systems at Hanford : a summary tabulation / (Richland, Wash. : U.S. Atomic Energy Commission, 1961), by D. E. Wood, United States. National Bureau of Standards. UC., United States. Department of Energy. Office of Fusion Energy. UC., United States. National Bureau of Standards. Fracture and Deformation Division. UC., U.S. Atomic Energy Commission. AEC research and development report, United States. Energy Research and Development Administration. TID., U.S. Atomic Energy Commission. TID., Hanford Works, and Hanford Atomic Products Operation (page images at HathiTrust)
• Calculated critical parameters for slightly enriched uranium rods in light water / (Richland, Wash. : U.S. Atomic Energy Commission, 1961), by C. L. Brown, United States. National Bureau of Standards. UC., United States. Department of Energy. Office of Fusion Energy. UC., United States. National Bureau of Standards. Fracture and Deformation Division. UC., U.S. Atomic Energy Commission. AEC research and development report, United States. Energy Research and Development Administration. TID., U.S. Atomic Energy Commission. TID., 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 / (Richland, Wash. : U.S. Atomic Energy Commission, 1961), by C. L. Brown, United States. National Bureau of Standards. UC., United States. Department of Energy. Office of Fusion Energy. UC., United States. National Bureau of Standards. Fracture and Deformation Division. UC., U.S. Atomic Energy Commission. AEC research and development report, United States. Energy Research and Development Administration. TID., U.S. Atomic Energy Commission. TID., Hanford Works, and Hanford Atomic Products Operation (page images at HathiTrust)
• Buckling of light water lattices (.600" diameter rods, 1.3% and 1.15% 25) / (Oak Ridge, Tenn. : United States Atomic Energy Commission, Technical Information Service, [1953]), 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 / (Oak Ridge, Tenn. : 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)
• A Koiter-type method for finite element analysis of nonlinear structural behavior. (Wright-Patterson Air Force Base, Ohio : 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 sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Effect of fiber orientation on initial postbuckling behavior and imperfection sensitivity of composite cylindrical shells / (Wright-Patterson Air Force Base, Ohio : 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 Koiter-type method for finite element analysis of nonlinear structural behavior. (Wright-Patterson Air Force Base, Ohio : 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 sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• An investigation of column action during creep buckling /, by R. L. Carlson, G. K. Manning, W. W. Breindel, sponsor Aerospace Research Laboratories (U.S.), sponsor United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command. issuing body, and sponsor Battelle Memorial Institute (page images at HathiTrust)
• Panel optimization with integrated software (POIS)., by D. Bushnell, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Lockheed Missiles and Space Company (page images at HathiTrust)
• Panel optimization with integrated software (POIS)., by P. Stern, P. Stehlin, Bo O. Almroth, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Lockheed Missiles and Space Company (page images at HathiTrust)
• General instability of orthotropically stiffened cylinders., by C. Lakshmikantham, Roger Milligan, George Gerard, sponsor Allied Research Associates, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• General instability of orthotropically stiffened cylinders., by Roger Milligan, Herbert Becker, C. Lakshmikantham, George Gerard, sponsor Allied Research Associates, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Development of experimental testing programs to verify thermal stress analysis /, by B. E. Gatewood, B. H. Ulrich, A. R. Glaser, sponsor Ohio State University. Department of Aeronautical and Astronautical Engineering, and sponsor 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 /, by Megumi Sunakawa, R. M. Evan-Iwanowski, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Syracuse University. Research Institute (page images at HathiTrust)
• A translation of flexible plates and shells /, by A. S. Volʹmir, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Florida. Department of Engineering Sciences (page images at HathiTrust)
• A study of the effects of penetration framing on steel containment buckling capacity / (Washington, D.C. : Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission : Available from Superintendent of Documents, U.S. Government Printing Office ; Springfield, Va. : National Technical Information Service, 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 / (Washington, D.C. : National Advisory Commitee for Aeronautics, [1938]), by G. Limpert and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• A Numerical approach to the instability problem of monocoque cylinders / (Washington, D.C. : 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)
• The effect of buckling on the multigroup diffusion theory group constants calculated by the MUFT code /, by R. S. Wick, U.S. Atomic Energy Commission, Westinghouse Electric Corporation, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Study of instantaneous collapse and creep buckling characteristics of large SGR process tubes / (Canoga Park, California : Atomics International, [1965]), by M. Lemcoe, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Extension of the safe geometric parameters to slightly enriched uranium / (Oak Ridge, Tenn. : 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)
• Experimental and numerical analysis of axially compressed circular cylindrical fiber-reinforced panels with various boundary conditions /, by Nelson R. Bauld, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and sponsor Clemson University. Department of Mechanical Engineering (page images at HathiTrust)
• Buckling of composites under hot and wet environment /, by V. Sarma Avva, L. Sharpe, D. Yogi Goswami, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor North Carolina Agricultural and Technical State University (page images at HathiTrust)
• Matrix analysis of shells : small and large displacements /, by J. H. Argyris, P. C. Patton, K. E. Buck, W. Bosshard, and issuing agency Air Force Flight Dynamics Laboratory (U.S.), ed. by J. B. Spooner (page images at HathiTrust)
• Stability of filament wound cylinders under combined loading /, by A. Holston, D. A. Stang, A. Feldman, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Martin Marietta Denver Aerospace (page images at HathiTrust)
• Dynamic buckling of shell structures subject to longitudinal impact /, by A. P. Coppa, W. A. Nash, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor General Electric Company (page images at HathiTrust)
• Optimality criteria in structural design /, by William Prager, Pedro V. Marcal, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Brown University. Division of Engineering (page images at HathiTrust)
• Collapse analysis for shells of general shape., by Bo O. Almroth, M. B. Marlowe, F. A. Brogan, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed Palo Alto Research Laboratory (page images at HathiTrust)
• Collapse analysis for shells of general shape. Volume 2. User's manual for the STAG-A computer code /, by Bo O. Almroth, H. T. Petersen, F. Zele, E. Meller, F. A. Brogan, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed Palo Alto Research Laboratory (page images at HathiTrust)
• A technique for obtaining improved real-time holographic interferometric data using pulse modulated illumination /, by Frank D. Adams, Gene E. Maddux, and issuing agency Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Investigation of the creep buckling behavior of columns :, by Ralph Papirno, George Gerard, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor New York University (page images at HathiTrust)
• Investigation of the creep buckling behavior of columns:, by Ralph Pairno, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor New York University (page images at HathiTrust)
• An investigation of the creep buckling behavior of columns :, by George Gerard, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor New York University (page images at HathiTrust)
• Correlation of plate creep buckling theory with experiments on long plates of aluminum alloy 2024-0 at 500° F /, by Ralph Papirno, George Gerard, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and sponsor New York University (page images at HathiTrust)
• Thermal buckling /, by Frederick V. Pohle, Irwin Berman, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and Polytechnic Institute of Brooklyn. |b Department of Aeronautical Engineering and Applied Mechanics. sponsor (page images at HathiTrust)
• BUCKDEL v 0.9 users and theory manuals : buckling and delamination analysis of stiffened laminated plates /, by Daniel S. Pipkins, Satya N. Atluri, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Implementation of a damage tolerance module into ASTROS /, 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., by Ravi B. Deo, Erdogan Madenci, B. L. Agarwal, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Design Methodology and Life Analysis of Postbuckled Metal and Composite Panels: Design Guide. Volume III /, by Ravi B. Deo, B. L. Agarwal, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Design development and durability validation of postbuckled composite and metal panels: technology assessment /, by Ravi B. Deo, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Buckling of thin-walled cylinder under axial compression and internal pressure / (Washington, D.C. : 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)

More items available under narrower terms.