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Shells (Engineering) -- Computer programs

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• Shells (Engineering)
• Elastic plates and shells -- Computer programs
• Structural analysis (Engineering) -- Computer programs
• Computer programs

• Shells (Engineering) -- Testing -- Computer programs
• Shells (Engineering) -- Thermal properties -- Computer programs

• Numerical nonlinear inelastic analysis of stiffened shells of revolution (National Aeronautics and Space Administration ;, 1975), by V. Svalbonas, P. Ogilvie, Harold Levine, and Grumman Aerospace Corporation (page images at HathiTrust)

• User document for computer programs for ring-stiffened shells of revolution (National Aeronautics and Space Administration ;, 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)

• A digital computer method for design and analysis of axisymmetric thin shells subjected to pressure and thermal environments (Los Alamos Scientific Laboratory of the University of California, 1964), by J. W. Neudecker, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)

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

• Candela, the Shell Builder (New York, Reinhold Pub. Corp., c1963), by Colin Faber, contrib. by O. N. Arup (page images at HathiTrust)
• Nonlinear Theories for Thin Shells (Cambridge, MA: Division of Engineering and Applied Physics, Harvard University, 1961), by J. Lyell Sanders
  • page images at HathiTrust
  • PDF at dtic.mil
• Fitting & welding cylinders (U.S. Dept. of Transportation, Maritime Administration, 1985), by Stephen L. Roggendorff and National Shipbuilding Research Program (page images at HathiTrust)
• Buckling criteria and application of criteria to design of steel containment shell : final report, January 1978 - March 1979 (Division of Systems Safety, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission;, 1979), by Paul Seide, S. F. Masri, V. Weingarten, U.S. Nuclear Regulatory Commission. Division of Systems Safety, and International Structural Engineers (page images at HathiTrust)
• Some elementary principles of shell stress analysis with notes on the use of the shear center (National Advisory Committee for Aeronautics, 1939), by Paul Kuhn and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculation of load distribution in stiffened cylindrical shells (National Advisory Commitee for Aeronautics, 1938), by Hans Ebner, H. Koller, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The strength of shell bodies - theory and practice (National Advisory Commitee for Aeronautics, 1937), by H. Ebner and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• Rectangular shell plating under uniformly distributed hydrostatic pressure (National Advisory Commitee for Aeronautics, 1940), by M. Neubert, A. Sommer, 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)
• Finite element analysis of translational shells (University of Illinois, 1970), by Tzu-cheng Chu, W. C. Schnobrich, and United States. Office of Naval Research (page images at HathiTrust)
• Behavior of a bi-material cylinder, including the effects of fracture (University of New Mexico, Bureau of Engineering Research], 1969), by Roy L. Johnson (page images at HathiTrust; US access only)
• Compressive strength of ship hull girders (Ship Structure Committee ;, 1977), by H. Becker, A. Coloa, Sanders Associates, and United States. Naval Sea Systems Command (page images at HathiTrust)
• Transient temperature fields in shells (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), by Mikhail Dimitrov Mikhaĭlov (page images at HathiTrust; US access only)
• Survey of investigations on the theory of flexible plates and shells (covering the period from 1941 to 1957) (National Aeronautics and Space Administration, 1963), by A. S. Volʹmir (page images at HathiTrust)
• On the state of stress near curvilinear holes in shells (National Aeronautics and Space Administration :, 1966), by Guriĭ Nikolaevich Savin and Guz,́ A. N. (page images at HathiTrust; US access only)
• A computer program for anisotropic shallow-shell finite elements using symbolic integration (U.S. National Aeronautics and Space Administration ;, 1976), by C. M. Andersen, John T. Bowen, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Finite element solution for thin shells of revolution (National Aeronautics and Space Administration :, 1964), by Z. A. Lu, E. P. Popov, J. Penzien, United States National Aeronautics and Space Administration, and Berkeley University of California (page images at HathiTrust)
• Structural synthesis of a stiffened cylinder (National Aeronautics and Space Administration, 1968), by William M. Morrow and Lucien A. Schmit (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 (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 (National Aeronautics and Space Administration, 1967), by Shigeo Kobayashi (page images at HathiTrust; US access only)
• Random pressure excitation of shells and statistical dependence effect of normal mode response (National Aeronautics and Space Administration, 1965), by Robert E. Davis (page images at HathiTrust; US access only)
• Flexural vibrations of the prestressed toroidal shell (National Aeronautics and Space Administration, 1965), by Artis A. Liepins (page images at HathiTrust; US access only)
• Spinning spherical shell (NASA ;, 1965), by W. P. Brown, Hughes Aircraft Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Geometrical and inertial properties of a class of thin shells of a general type (National Aeronautics and Space Administration, 1965), by Will J. Worley and Han-chung Wang (page images at HathiTrust; US access only)
• Analytical and experimental investigation of pressurized toroidal shells (National Aeronautics and Space Administration, 1965), by P. F. Jordan (page images at HathiTrust; US access only)
• A theory of anisotropic viscoelastic sandwich shells (National Aeronautics and Space Administration, 1966), by John L. Baylor, United States National Aeronautics and Space Administration, and Berkeley University of California (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; US access only)
• Almost sure stability of long cylindrical shells with random imperfections (National Aeronautics and Space Administration, 1968), by Rena Scher Fersht (page images at HathiTrust; US access only)
• An experimental investigation of the radial displacements of a thin-walled cylinder (National Aeronautics and Space Administration, 1967), by O. G. S. Ricardo (page images at HathiTrust; US access only)
• Buckling of conical shells under axial compression (National Aeronautics and Space Administration, 1968), by Johann Arbocz (page images at HathiTrust; US access only)
• Analysis of a spherical shell with a non-axisymmetric boundary (National Aeronautics and Space Administration, 1966), by Z. M. Elias and P. K. Ho (page images at HathiTrust; US access only)
• The flutter of flexible, towed tension shells (National Aeronautics and Space Administration, 1967), by Richard H. MacNeal (page images at HathiTrust; US access only)
• Vibration of skewed cantilever plates and helicoidal shells (National Aeronatics and Space Administration, 1975), by D. P. Beres, C. D. Bailey, Ohio State University, and Langley Research Center (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)
• Stress, stability, and vibration of complex branched shells of revolution : analysis and user's manual for BOSOR4 (National Aeronautics and Space Administration :, 1972), by D. Bushnell (page images at HathiTrust)
• Analysis of large bending deformations of a filamentary tubular shell typical for pressure constraint components of space suits (National Aeronautics and Space Administration ;, 1970), by Odus R. Burggraf and Astro Research Corporation (page images at HathiTrust)
• A review of analytical methods used to determine the modal characteristics of cylindrical shells (National Aeronautics and Space Administration, 1966), by Kevin Forsberg (page images at HathiTrust; US access only)
• 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)
• Analysis of laminated, composite, circular cylindrical shells with general boundary conditions (National Aeronautics and Space Administration, 1974), by S. Srinivas and Langley Research Center (page images at HathiTrust)
• NASA TN D-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; US access only)
• NASA TR R-227 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), by David A. Evensen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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; US access only)
• NASA TN D-3543 (National Aeronautics and Space Administration :, 1966), by Joseph Edward Walz and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Shear-flexible finite-element models of laminated composite plates and shells (National Aeronautics and Space Administration ;, 1975), by Ahmed Khairy Noor, Michael D. Mathers, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6471 (National Aeronautics and Space Administration :, 1971), by Robert J. Platt, Marvin D. Rhodes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An engineering procedure for calculating compressive strength of isogrid cylindrical shells with buckled skin (National Aeronautics and Space Administration ;, 1976), by Walter L. Heard, Paul Slysh, Melvin S. Anderson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3066 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Robert Miserentino, Louis F. Vosteen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Membrane analysis of scalloped shells (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Ravindra K. Vyas (page images at HathiTrust; US access only)
• NASA TN D-5636 (National Aeronautics and Space Administration :, 1970), by James Wayne Sawyer, Langley Research Center, and United States National Aeronautics and Space Administration (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; US access only)
• NASA TN D-5701 (National Aeronautics and Space Administration ;, 1970), by George E. Weeks, Joseph E. Waltz, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5663 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by John L. Sewall, Donnell S. Catherines, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1692 (National Aeronautics and Space Administration, 1962), by H. U. Schuerch, A. C. Kyser, O. R. Burggraf, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1741 (National Aeronautics and Space Administration, 1963), by David A. Spera, Robert H. Johns, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1690 (National Aeronautics and Space Administration, 1962), by H. U. Schuerch, G. M. Schindler, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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; US access only)
• NASA TN D-6340 (National Aeronautics and Space Administration ;, 1971), by W. E. Zorumski, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 (National Aeronautics and Space Administration, 1959), by Cornelius Driver and Langley Research Center (page images at HathiTrust)
• A theoretical study of the rotary sizing of uranium tube (Battelle Memorial Institute ;, 1962), by Edward G. Bodine, Stan J. Paprocki, Edward G. Smith, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• The effect of end conditions on the dynamic response of cylindrical shells (Armour Research Foundation, Illinois Institute of Technology, 1960), by R. L. Chiapetta, Philip Gibson Hodge, U.S. Atomic Energy Commission, and Armour Research Foundation (U.S.) (page images at HathiTrust; US access only)
• Investigation of a corrugated shell as an elastic support of a bundle of rods (General Electric, Nuclear Materials and Propulsion Operation, 1961), by J. H. Meier, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Plastic instability of cylindrical shells with rigid end closures : topical report (Washington D.C., : Db Technical Services, Department of Commerce ; Dc [1962]., 1962), by M. A. Salmon, IIT Research Institute, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Static loading of MX model closures : final report (U.S. Army Engineer Waterways Experiment Station, 1979), by James V. Getchell, James M. Watt, and United States. Defense Nuclear Agency (page images at HathiTrust)
• Subscale MX Shelter Closure Structural Response Test Program : Report 1: Phases I and II closure static tests (The Station, 1982), by Paul S. Eagles, Gayle E. Albritton, Structures Laboratory (U.S.), and United States. Air Force. Ballistic Missile Office (page images at HathiTrust)
• Inelastic stress in a long cylindrical shell under a band of pressure (Atomics International, 1962), by T. C. Yen, W. F. Anderson, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Flexural characteristics of radially loaded cylindrical shells with stiffening rings (Sandia Corporation ;, 1961), by D. R. Fisher and Sandia Corporation (page images at HathiTrust)
• Fabrication of zirconium shells... (in the 20th century), by R. S. Pratt, C. H. Mayer, R. S. French, Inc Sylvania Electric Products, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Seal-shell-2 : a computer program for the stress analysis of a thick shell of revolution with axisymmetric pressures, temperatures, and distributed loads (Washington, D.C. : Office of Technical Services, Department of Commerce, 1963., 1963), by C. M. Friedrich, Bettis Atomic Power Laboratory, Westinghouse Electric Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Structure design notes : calculation of stresses, forces, and deflections in linear-elastic skeleton structures with temperature, pressures, applied loads and redundant loads (Washington, D.C. : Office of Technical Services, Department of Commerce, 1964., 1964), by C. M. Friedrich, Bettis Atomic Power Laboratory, Westinghouse Electric Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Design, construction and testing of a Masonite triboloid shell structure (School of Engineering and Architecture, University of Kansas, 1964), by William B. Duncan and Willard Strode (page images at HathiTrust; US access only)
• Stresses and deformations of an elastically supported cylindrical shell (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by R. T. Gray, G. Horvay, W. A. Boothe, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Analysis of short cylindrical and conical shell sections (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by C. Linkous, G. Horvay, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachment. Part I, Summary of the investigation (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by N. J. Hoff, F. V. Pohle, S. V. Nardo, J. Kempner, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachment. Part II, Line loads acting along generatrices of circular cylindrical shells (Schenectady, New York : Knolls Atomic Power Laboratory, 1952., 1952), by N. J. Hoff, F. V. Pohle, J. Kempner, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachment. Part III, Numerical methods (Schenectady, New York : Knolls Atomic Power Laboratory, 1952., 1952), by Frederick V. Pohle, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachment. Part IV, Work charts (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by J. Kempner, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachments. Part V, Local effect of the pipe (Schenectady, New York : Knolls Atomic Power Laboratory, 1952., 1952), by N. J. Hoff, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachment. Part VI, Derivation of generalized donnell-type equations for circular cylindrical shells with application to shells with line loads along generatrices (Schenectady, New York : Knolls Atomic Power Laboratory, 1953., 1953), by J. Kempner, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Collapsible tube industry (United States Government Printing Office, 1934), by United States National Recovery Administration (page images at HathiTrust)
• Collapsible tube industry (United States Government Printing Office, 1934), by United States National Recovery Administration (page images at HathiTrust)
• Static nonlinear analysis of shells of revolution users manual (Albuquerque, New Mexico : Sandia Corporation, Aero-Thermodynamics Department, 1968., 1968), by Walter E. Haisler, James A. Stricklin, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Experimental investigation of creep bending and buckling of thin circular cylindrical shells (National Advisory Committee for Aeronautics, 1957), by Burton Erickson and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Influence coefficients for circular cylindrical shellswith linearly varying wall thickness (Washington, D.C. : United States Air Force, Office of Scientific Research, Mathematics Division, 1957., 1957), by Marvin Banks Sledd, United States. Air Force. Office of Scientific Research, and Georgia Institute of Technology. Engineering Experiment Station (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)
• 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)
• Statics and stability of thin-walled elastic beams. Part 1, Formulation of fundamental equations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by E. Giangreco, M. Como, M. Capurso, Università di Napoli, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Statics and stability of thin-walled elastic beams. Part 2, Solution of equations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by E. Giangreco, M. Como, M. Capurso, Università di Napoli, and Air Force Flight Dynamics Laboratory (U.S.) (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)
• An automated procedure for the optimization of practical aerospace structures. Volume 1, Theoretical development and user's information (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamicsl Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by Walter J. Dwyer, Irving U. Ojalvo, Robert K. Emerton, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Grumman Aerospace Corporation (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)
• MAGIC : n automated general purpose system for structural analysis. Volume 1, Engineer's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by Robert H. Mallett, Stephen Jordan, Air Force Flight Dynamics Laboratory (U.S.), and Bell Aerospace Textron (page images at HathiTrust)
• Techniques for measuring displacement fields of deformed bodies using holographic interferometry (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Mechanics Branch, Structures Division, Air Force Systems Command, United States Air Force, 1971., 1971), by Gene E. Maddux, R. R. Corwin, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• An assessment of current capability for computer analysis of shell structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by Richard F. Hartung, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed Palo Alto Research Laboratory (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)
• Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 3, Experimental evaluation of the general time-dependent analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by R. J. Edwards, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
• MAGIC : an automated general purpose system for structural analysis. Volume 2, User's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by Stephen Jordan, Air Force Flight Dynamics Laboratory (U.S.), Bell Aerospace Textron, Robert H. Mallett, and Gene E. Maddux (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)
• Structural response of a shallow spherical shell (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by James L. Rudd, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (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)
• Thermo-structural analysis manual. Volume II (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1962., 1962), by Marvin J. Forray, M. Noiman, H. Switzky, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and Republic Aviation Corporation (page images at HathiTrust)
• Buckling and post-buckling behavior of axially-compressed cylindrical shells subjected to internal pressure (Urbana : Illinois : University of Illinois, Department of Theoretical and Applied Mechanics, July, 1957., 1957), by H. L. Langhaar, University of Illinois at Urbana-Champaign. Department of Theoretical and Applied Mechanics, and United States. Office of Naval Research. Department of Navy (page images at HathiTrust; US access only)
• Analysis of structural shells with transverse shear deformation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by RIchard L. Citerley, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Inc Anamet Laboratories (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)

More items available under broader and related terms at left.