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Shells (Engineering)

Here are entered works on shells as engineering structures. Works on the mathematical theories of elasticity in plates and shells are entered under Elastic plates and shells. Works on plates as engineering structures are entered under Plates (Engineering).

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

• Elastic plates and shells
• Structural analysis (Engineering)

• Plates (Engineering)

• Blades
• Conical shells
• Noses (Aircraft)
• Planing hulls
• Roofs, Shell
• Shells, Concrete
• Tanks
• Tubes

• Structural shells

• 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
• Thermal distortions of thin-walled paraboloidal shells / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1966), by Joseph Edward Walz and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Cornelius Driver and Langley Research Center (page images at HathiTrust)
• Behavior of a bi-material cylinder, including the effects of fracture (Albuquerque, University of New Mexico, Bureau of Engineering Research], 1969), by Roy L. Johnson (page images at HathiTrust; US access only)
• User document for computer programs for ring-stiffened shells of revolution / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)
• Automated shell theory for rotating structures (astros) (Washington, National Aeronautics and Space Administration [For sale by the National Technical Information Service, Springfield, Va.], 1971), by Byron J. Foster, Jerrell M. Thomas, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Code of fair competition for the collapsible tube industry as approved on March 17, 1934. (Washington, D.C. : United States Government Printing Office, 1934), by United States National Recovery Administration (page images at HathiTrust)
• Amendment to code of fair competition for the collapsible tube industry as approved on August 29, 1934. (Washington, D.C. : United States Government Printing Office, 1934), by United States National Recovery Administration (page images at HathiTrust)
• Small oscillations of thin resilient conical shells / (Washington : National Aeronautics and Space Administration, 1960), by Ėduard Ivanovich Grigoli︠u︡k (page images at HathiTrust)
• Stress, stability, and vibration of complex branched shells of revolution : analysis and user's manual for BOSOR4 / (Washington : National Aeronautics and Space Administration : Springfield, Va. : distributed by National Technical Information Service, 1972), by D. Bushnell (page images at HathiTrust)
• A finite element for thermal stress analysis of shells of revolution / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Howard M. Adelman, James L. Rogers, Harold C. Lester, and Langley Research Center (page images at HathiTrust)
• Elevated-temperature tests under static and aerodynamic conditions on corrugated-stiffened panels / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Joseph M. Groen, Richard Rosecrans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of large bending deformations of a filamentary tubular shell typical for pressure constraint components of space suits / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Odus R. Burggraf and Astro Research Corporation (page images at HathiTrust)
• Analysis of laminated, composite, circular cylindrical shells with general boundary conditions / (Washington, D.C. : National Aeronautics and Space Administration, 1974), by S. Srinivas and Langley Research Center (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)
• Finite element solution for thin shells of revolution / (Washington : National Aeronautics and Space Administration : Springfield, Va. : for sale by the National Technical Information Service, 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)
• On the prediction of the vibratory behavior of free-free truncated conical shells / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Eugene C. Naumann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical nonlinear inelastic analysis of stiffened shells of revolution / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by National Technical Information Service, 1975), by V. Svalbonas, P. Ogilvie, Harold Levine, and Grumman Aerospace Corporation (page images at HathiTrust)
• Computer analysis of ring-stiffened shells of revolution / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (page images at HathiTrust)
• Axisymmetric oscillation of a partially liquid-filled cylindrical shell container having hemispherical bulkheads / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Rudolf F. Glaser and George C. Marshall Space Flight 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)
• Temperature distribution in a spinning spherical shell in the solar flux uniformly valid perturbation expansion for a thin shell / (Washington : NASA ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by W. P. Brown, Hughes Aircraft Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Shear-flexible finite-element models of laminated composite plates and shells / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Ahmed Khairy Noor, Michael D. Mathers, and Langley Research Center (page images at HathiTrust)
• Stability analysis of plates and shells : a collection of papers in honor of Dr. Manuel Stein / (Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1998), by Manuel Stein, Michael P. Nemeth, Norman F. Knight, Langley Research Center, and Structural Dynamics AIAA/ASME/ASCE/AHS/ASC Structures (page images at HathiTrust)
• Experimental investigation of creep bending and buckling of thin circular cylindrical shells / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Burton Erickson and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Design, construction and testing of a Masonite triboloid shell structure, (Lawrence, School of Engineering and Architecture, University of Kansas, 1964), by William B. Duncan and Willard Strode (page images at HathiTrust; US access only)
• 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)
• Stability, fatigue and optimization of thin-walled structures under cryogenic conditions : application in the structural design of colliders and cryogenic transfer lines / (Geneva : CERN, 2001), by B Skoczen and European Organization for Nuclear Research. Large Hadron Collider Division (page images at HathiTrust)
• An experimental and analytical vibration study of thin cylindrical shells with and without longitudinal stiffeners, ([Washington] National Aeronautic and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1968]), by John L. Sewall and Eugene C. Naumann (page images at HathiTrust; US access only)
• Vibrations of a hollow elastic cylinder bonded to a thin casing of a different material / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Vasant S. Kelkar, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Free vibrations of conical shells / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, U.S. G.P.O.], 1965), by William C. L. Hu and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A theory and applications of filamentary structures / (Washington, D.C. : 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)
• An experimental and analytical vibration study of elliptical cylindrical shells / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by John L. Sewall, Christine G. Pusey, William M. Thompson, Langley Research Center, and United States National Aeronautics and Space Administration (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 / (Washington : National Aeronautics and Space Administration, 1962), by V. V. Bolotin (page images at HathiTrust; US access only)
• Vibration tests of pressurized thin-walled cylindrical shells / (Washington, D.C. : 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)
• A contribution to the theory of folding deformations in expandable structures with a particular application to toroidal shells / (Washington, D.C. : 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)
• Compressive strength of ship hull girders / (Washington : Ship Structure Committee ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by H. Becker, A. Coloa, Sanders Associates, and United States. Naval Sea Systems Command (page images at HathiTrust)
• Vibration of shells (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1973), by Arthur W. Leissa (page images at HathiTrust)
• A computer program for anisotropic shallow-shell finite elements using symbolic integration / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by C. M. Andersen, John T. Bowen, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Vibration of skewed cantilever plates and helicoidal shells / (Washington, D.C. : National Aeronatics and Space Administration, 1975), by D. P. Beres, C. D. Bailey, Ohio State University, and Langley Research Center (page images at HathiTrust)
• Stress concentration in a cylindrical shell with a round aperture in its side / ([Washington, D.C. : ] National Aeronautics and Space Administration, [1964]), by I︠U︡. A. Shevli︠a︡kov (page images at HathiTrust)
• Survey of investigations on the theory of flexible plates and shells (covering the period from 1941 to 1957) / (Washington, DC : National Aeronautics and Space Administration, 1963), by A. S. Volʹmir (page images at HathiTrust)
• Free oscillations of circular conical and cylindrical shells reinforced by rigid circular ribs / (Washington, D.C. : National Aeronautics and Space Administration, [1965]), by V. G. Godzevich and O. V. Ivanova (page images at HathiTrust)
• The stressed state near curvilinear reinforced orifices in shells / ([Washington, D.C. :] National Aeronautics and Space Administration, [1966]), by Aleksandr Nikolaevich Guzʹ and Guriĭ Nikolaevich Savin (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)
• Transient response of shells of revolution by direct integration and modal superposition methods / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Wendell B. Stephens, Howard M. Adelman, and Langley Research Center (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 theory of anisotropic viscoelastic sandwich shells / (Washington, D. C. : 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)
• Computer analysis of multicircuit shells of revolution by the field method / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Gerald A. Cohen, Langley Research Center, and Structures Research Associates (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)
• Thermal distortion of a paraboloidal shell / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Robert J. Platt, Marvin D. Rhodes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical and experimental studies of natural vibration modes of ring-stiffened truncated-cone shells with variable theoretical ring fixity / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Eugene C. Naumann, William C. Walton, Donnell S. Catherines, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nonlinear flexural vibrations of thin-walled circular cylinders / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by David A. Evensen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Diffracted and head waves associated with waves on nonseparable surfaces / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Raymond L. Barger and Langley Research Center (page images at HathiTrust)
• A triangular thin shell finite element : linear analysis / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by G. R. Thomas, Richard H. Gallagher, Langley Research Center, and Cornell University (page images at HathiTrust)
• A triangular thin shell finite element : nonlinear analysis / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by G. R. Thomas, Richard H. Gallagher, Langley Research Center, and Cornell University (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)
• 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)
• Longitudinal-transverse bending of stiffened circular cylindrical shells / (Washington, D.C. : National Aeronautics and Space Administration, [1964]), by Saveliĭ Nakhimovich Kan and D. Ye Lipovskiy (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)
• Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at Mach 3.0 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by James Wayne Sawyer, William D. Deveikis, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation of temperature distributions in thin shells of revolution by the finite-element method / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Howard M. Adelman, Donnell S. Catherines, 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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• Effects of pressure distributions on bluff tension-shell shapes / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and technical Information, Springfield, Va. 22151], 1970), by James Wayne Sawyer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Generalized ring stiffness matrix for ring-stiffened shells of revolution / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by George E. Weeks, Joseph E. Waltz, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical vibration study of a ring-stiffened conical shell and comparison with experiment / (Washington, D.C. : 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)
• Supersonic aerodynamics of large-angle cones / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by James F. Campbell, Dorothy T. Howell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A method for computation of vibration modes and frequencies of orthotropic thin shells of revolution having general meridional curvature / (Washington, D.C. : National Aeronautics and Space Administration, 1969), by Howard M. Adelman, William C. Walton, Donnell S. Catherines, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Acoustic scattering and absorption by a rigid porous elliptic cylindrical shell / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by W. E. Zorumski, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Finite element analysis of translational shells, (Urbana, University of Illinois, 1970), by Tzu-cheng Chu, W. C. Schnobrich, and United States. Office of Naval Research. cn (page images at HathiTrust)
• On the state of stress near curvilinear holes in shells / (Washington : National Aeronautics and Space Administration : For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, VA, 1966), by Guriĭ Nikolaevich Savin and Guz,́ A. N. (page images at HathiTrust; US access only)
• Membrane analysis of scalloped shells, ([Washington] 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)
• 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)
• Theoretical elastic stress distributions in Cassinian domes / (Washington, D.C. : 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)
• 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)
• Structural synthesis of a stiffened cylinder / (Washington, D.C. : 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 / (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)
• Random pressure excitation of shells and statistical dependence effect of normal mode response / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by Robert E. Davis (page images at HathiTrust; US access only)
• Flexural vibrations of the prestressed toroidal shell / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by Artis A. Liepins (page images at HathiTrust; US access only)
• Flexural vibrations of conical shells with free edges / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by W. C. L. Hu, U. S. Lindholm, and J. F. Gormley (page images at HathiTrust; US access only)
• Geometrical and inertial properties of a class of thin shells of a general type / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by P. F. Jordan (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)
• 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)
• An experimental investigation of the radial displacements of a thin-walled cylinder / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by O. G. S. Ricardo (page images at HathiTrust; US access only)
• On the differential equations of the axisymmetric vibration of paraboloidal shells of revolution / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by James Ting-shun Wang and Chi-wen Lin (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)
• Analysis of a spherical shell with a non-axisymmetric boundary / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Richard H. MacNeal (page images at HathiTrust; US access only)
• A review of analytical methods used to determine the modal characteristics of cylindrical shells / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Kevin Forsberg (page images at HathiTrust; US access only)
• Vibration study of a pressurized torus shell / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Peter F. Jordan and Atis A. Liepins (page images at HathiTrust; US access only)
• Effect of shallow meridional curvature on the vibration of nearly cylindrical shells / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Paul A. Cooper, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Transient temperature fields in shells, ([Washington] 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)
• The strength of shell bodies - theory and practice / (Washington, D.C. : National Advisory Commitee for Aeronautics, [1937]), by H. Ebner and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• Buckling criteria and application of criteria to design of steel containment shell : final report, January 1978 - March 1979 / (Washington, D.C. : Division of Systems Safety, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission; Springfield, Va. : Available from National Technical Information Service, 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)
• 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)
• Fitting & welding cylinders / ([Washington, D.C.?] : U.S. Dept. of Transportation, Maritime Administration, [1985]), by Stephen L. Roggendorff and National Shipbuilding Research Program (page images at HathiTrust)
• Some elementary principles of shell stress analysis with notes on the use of the shear center / (Washington, D.C. : National Advisory Committee for Aeronautics, 1939), by Paul Kuhn and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Rectangular shell plating under uniformly distributed hydrostatic pressure / (Washington, D.C. : National Advisory Commitee for Aeronautics, [1940]), by M. Neubert, A. Sommer, and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• A theoretical and experimental study of the nonlinear flexural vibrations of thin circular rings / (Washington, D.C. : 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)
• The effect of nonuniform temperature distributions on the stresses and distortions of stiffened-shell structures / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Richard R. Heldenfels and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The effect of end conditions on the dynamic response of cylindrical shells / (Chicago, Ill. : 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)
• Fabrication of zirconium shells..., by R. S. Pratt, C. H. Mayer, R. S. French, Inc Sylvania Electric Products, 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 /, by C. M. Friedrich, Bettis Atomic Power Laboratory, Westinghouse Electric Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Deformations and stresses in circular cylindrical shells caused by pipe attachment., 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., 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., 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 attachment., by M. T. Roche, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• A study of the vibrations of shallow spherical shells /, by W. H. Hoppmann, C. N. Baronet, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• A theoretical study of the rotary sizing of uranium tube / (Columbus, OH : Battelle Memorial Institute ; Washington, D.C. : Available from Office of Technical Services, U.S. Dept. of Commerce, [1962]), by Edward G. Bodine, Stan J. Paprocki, Edward G. Smith, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Richard R. Heldenfels and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A digital computer method for design and analysis of axisymmetric thin shells subjected to pressure and thermal environments / (Los Alamos, N.M. : 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)
• Investigation of a corrugated shell as an elastic support of a bundle of rods / (Cincinnati, Ohio : 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)
• Seal-shell : a digital program to determine stresses and deflections in an axisymmetric shell of revolution /, by C. M. Friedrich, Westinghouse Electric Corporation, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (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 /, by C. M. Friedrich, Bettis Atomic Power Laboratory, Westinghouse Electric Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Stresses and deformations of an elastically supported cylindrical shell /, 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 /, 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., 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 attachments., 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., by J. Kempner, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Response of submerged spherical shells to internal blast loading /, by W. E. Baker, J. D. Patterson, J. W. Hanna, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Static nonlinear analysis of shells of revolution users manual /, by Walter E Haisler, James A. Stricklin, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Bounds on influence coefficients for circular cylindrical shells /, by Eric Reissner, M. B. Sledd, United States. Air Force. Office of Scientific Research, and Georgia Institute of Technology. Engineering Experiment Station (page images at HathiTrust)
• Computer oriented analysis of shell structures : proceedings of a conference held at Palo Alto, California, August 10-14, 1970 /, by issuing agency Air Force Flight Dynamics Laboratory (U.S.) and sponsor Lockheed Missiles and Space Company, ed. by Richard F. Hartung (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)
• An automated procedure for the optimization of practical aerospace structures., by Walter J. Dwyer, Irving U. Ojalvo, Robert K. Emerton, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing body United States. Air Force. Systems Command, and sponsor Grumman Aerospace Corporation (page images at HathiTrust)
• Elasto-plastic analysis of structures under load and two-dimensional temperature distributions., by R. J. Edwards, issuing body United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.) sponsor, and sponsor Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
• Structural response of a shallow spherical shell /, by James L. Rudd, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Statics and stability of thin-walled elastic beams., by E. Giangreco, M. Como, M. Capurso, sponsor Università di Napoli, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Statics and stability of thin-walled elastic beams., by E. Giangreco, M. Como, M. Capurso, sponsor Università di Napoli, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (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)
• MAGIC : an automated general purpose system for structural analysis., by Stephen Jordan, issuing agency Air Force Flight Dynamics Laboratory (U.S.), sponsor Bell Aerospace Textron, Robert H. Mallett, and Gene E. Maddux (page images at HathiTrust)
• Limit analysis of rotationally symmetric plates and shells. (Englewood Cliffs, N. J. : Prentice-Hall, 1963), by Philip Gibson Hodge (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].), 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 / (Vicksburg, Miss. : 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)
• Influence coefficients for circular cylindrical shellswith linearly varying wall thickness /, by Marvin Banks Sledd, United States. Air Force. Office of Scientific Research, and Georgia Institute of Technology. Engineering Experiment Station (page images at HathiTrust)
• Subscale MX Shelter Closure Structural Response Test Program : Report 1: Phases I and II closure static tests / (Vicksburg, Miss. : 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 / (Canoga Park, California : 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 / ([Albuquerque, N.M.] : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [1961]), by D. R. Fisher and Sandia Corporation (page images at HathiTrust)
• An assessment of current capability for computer analysis of shell structures /, by Richard F. Hartung, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed Palo Alto Research Laboratory (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)
• MAGIC : n automated general purpose system for structural analysis., by Robert H. Mallett, Stephen Jordan, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Bell Aerospace Textron (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)
• Techniques for measuring displacement fields of deformed bodies using holographic interferometry /, by Gene E. Maddux, R. R. Corwin, and issuing agency Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Thermo-structural analysis manual., by Marvin J. Forray, M. Newman, H. Switzky, issuing body United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and sponsor Republic Aviation Corporation (page images at HathiTrust)

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