Plates (Engineering)Here are entered works on plates as engineering structures. Works on shells as engineering structures are entered under Shells (Engineering). Works on the mathematical theories of elasticity in plates and shells are entered under Elastic plates and shells. See also what's at your library, or elsewhere.
Broader terms:Related term:Narrower terms:Used for:- Disks (Mechanics)
- Panels
- Structural plates
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Filed under: Plates (Engineering) Skew Plates and Structures (New York: Macmillan, 1963), by L. S. D. Morley (page images at HathiTrust) An Investigation of sheet-stiffener panels subjected to compression loads with particular reference to torsionally weak stiffeners (National Advisory Committee for Aeronautics, 1940), by Louis Dunn and United States National Advisory Committee 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) Probleme der Statik technisch wichtiger orthotroper Platten : Gastvorlesungen in der Eidgenössischen Technischen Hochschule Zürich, Februar 1929 (Nakładem Akademji nauk technicznych :, 1929), by M. T. Huber and Eidgenössische Technische Hochschule (page images at HathiTrust) Evaluation of bearing plates installed on full-column resin-grouted bolts (U.S. Dept. of the Interior, Bureau of Mines, 1986), by Stephen C. Tadolini and Bryan F. Ulrich (page images at HathiTrust) Die elastischen Platten : die Grundlagen und Verfahren zur Berechnung ihrer Formänderungen und Spannungen, sowie die Anwendungen der Theorie der ebenen zweidimensionalen elastischen Systeme auf praktische Aufgaben (Springer, 1925), by Arpád Nádai (page images at HathiTrust; US access only) Calculation of spall based on a one-dimensional model (Lawrence Radiation Laboratory, 1961), by Mark L. Wilkins and Lawrence Radiation Laboratory (page images at HathiTrust) Finite element techniques for orthotropic plane stress and orthotropic plate analysis (U.S. Dept. of Agriculture, Forest Products Laboratory, 1968), by A. Carl Maki (page images at HathiTrust) Some views on large structural particleboard panels (U.S. Dept. of Agriculture, Forest Service Forest Products Laboratory, 1972), by Bruce G. Heebink, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust) 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) Gross panel strength under combined loading (Ship Structure Committee ;, 1977), by A. E. Mansour, United States. Ship Structure Committee, NAVSEC (Organization : U.S.), and inc Mansour Engineering (page images at HathiTrust) 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) Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Dawn C. Jegley and Langley Research Center (page images at HathiTrust) Interstage adapter panel flutter on Atlas-Centaur AC-2, AC-3, and AC-4 vehicles (National Aeronautics and Space Administration ;, 1965), by Tilak R. Lall and Lewis Research Center (page images at HathiTrust) Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust) Analyses of surface cracks in finite plates under tension or bending loads (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by J. C. Newman, I. S. Raju, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by William L. Ko, Raymond H. Jackson, and Dryden Flight Research Facility (page images at HathiTrust) An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Michael P. Nemeth, Eric R. Johnson, Manuel Stein, and Langley Research Center (page images at HathiTrust) A cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by C. A. Bigelow and Langley Research Center (page images at HathiTrust) Fabrication and evaluation of cold-formed/weld-brazed beta-titanium skin-stiffened compression panels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Dick M. Royster and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) Boundary-layer transition on a plate subjected to simultaneous spanwise and chordwise pressure gradients (National Aeronautics and Space Administration ;, 1974), by Donald R. Boldman, Paul F. Brinich, and Lewis Research Center (page images at HathiTrust) Analysis of solar thermoelectric flat-plate generators operating in the range of 1.0 to 0.1 astronomical unit (National Aeronautics and Space Administration ;, 1966), by William J. Bifano and Lewis Research Center (page images at HathiTrust) Brazed Borsic/aluminum structural panels (National Aeronautics and Space Administration ;, 1977), by Thomas T. Bales, Dick M. Royster, H. Ross Wiant, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Manuel Stein, P. Daniel Sydow, Liviu Librescu, and Langley Research Center (page images at HathiTrust) Calculation procedure for transient heat transfer to a cooled plate in a heated stream whose temperature varies arbitrarily with time (National Aeronautics and Space Administration ;, 1975), by James Sucec and Lewis Research Center (page images at HathiTrust) A buckling analysis for rectangular orthotropic plates with centrally located cutouts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Michael P. Nemeth and Langley Research Center (page images at HathiTrust) Joining and fabrication of metal-matrix composite materials (National Aeronautics and Space Administration ;, 1975), by Dick M. Royster, Thomas T. Bales, H. Ross Wiant, and Langley Research Center (page images at HathiTrust) Buckling and failure characteristics of graphite-polyimide shear panels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Mark J. Shuart, Jane A. Hagaman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) Flow-induced vibrations of a flat plate suspended in a narrow channel (National Aeronautics and Space Administration, 1968), by Franklin T. Dodge and Arthur. F. Muller (page images at HathiTrust; US access only) Research on panel flutter (National Aeronautics and Space Administration, 1964), by D. R. Kobett (page images at HathiTrust; US access only) Dynamic characteristics of square plates by passive analog simulation (National Aeronautics and Space Administration ;, 1967), by R. L. Barnoski, George C. Marshall Space Flight Center, Measurement Analysis Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust) Control of the meteoroid hazard to space vehicles (National Aeronautics and Space Administration, 1964), by Philip J. D'Anna, James J. Piechocki, Roger M. Heitz, Northrop Space Laboratories, and United States National Aeronautics and Space Administration (page images at HathiTrust) Research study to provide concepts of panel attachment mechanisms suitable for refurbishable panel application (National Aeronautics and Space Administration ;, 1966), by R. E. Rieckmann, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Measurements of nonequilibrium effects in air on wedge-flat-plate afterbody pressures (National Aeronautics and Space Administration, 1965), by R. J. Vidal and F. Stoddard (page images at HathiTrust) The eigenvalue problem for beams and rectangular plates with linearly varying in-plane and axial load (For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by Guy Fauconneau and William M. Laird (page images at HathiTrust) Exploratory investigation of sound pressure level in the wake of an oscillating airfoil in the vicinity of stall (National Aeronautics and Space Administration ;, 1972), by Robin B. Gray, G. A. Pierce, Langley Research Center, and Georgia Institute of Technology (page images at HathiTrust) Flutter of multiple-streamwise bay rectangular panels at low supersonic mach number (National Aeronautics and Space Administration, 1966), by D. R. Kobett (page images at HathiTrust) A wind tunnel investigation of panel response to boundary layer pressure fluctuations at mach 1.4 and mach 3.5 (National Aeronautics and Space Administration, 1966), by David Alan Bies (page images at HathiTrust) NASA CR-1175 (National Aeronautics and Space Administration ;, 1968), by Anthony Craggs and United States National Aeronautics and Space Administration (page images at HathiTrust) 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) Small deflection of a class of clamped thin plates using conformal mapping (Dept. of Theoretical and Applied Mechanics, University of Illinois, 1970), by Will J. Worley, Thomas F. Moriarty, United States National Aeronautics and Space Administration, and University of Illinois at Urbana-Champaign. Dept. of Theoretical and Applied Mechanics (page images at HathiTrust) An analytical study of hydrogen cooled panels for application to hypersonic aircraft (National Aeronautics and Space Administrtion, 1971), by W. G. Flieder, Langley Research Center, Garrett Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust) Analysis of fatigue crack propagation (National Aeronautics and Space Administration ;, 1972), by H. W. Liu (page images at HathiTrust) Stresses at the tip of a longitudinal crack in a plate strip (National Aeronautics and Space Administration, 1967), by W. B. Fichter (page images at HathiTrust) 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) NASA TR R-166 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963), by W. Jefferson Stroud, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only) Supersonic flutter of panels loaded with inplane shear (National Aeronautics and Space Administration ;, 1975), by James Wayne Sawyer and Langely Research Center (page images at HathiTrust) NASA TN D-2227 (National Aeronautics and Space Administration, 1963), by D. R. Kobett, E. F. E. Zeydel, Mo.) Midwest Research Institute (Kansas City, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only) A study of stiffness matrices for the analysis of flat plates (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Dennis A. Kross (page images at HathiTrust) NASA TN D-4357 (National Aeronautics and Space Administration ;, 1968), by Robert W. Fralich, John A. McElman, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) 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-6479 (National Aeronautics and Space Administration :, 1971), by Gary L. Giles, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Analytical structural efficiency studies of borsic/aluminum compression panels (National Aeronautics and Space Administration ;, 1976), by Robert R. McWithey 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) Effects of eccentricities and lateral pressure on the design of stiffened compression panels (National Aeronautics and Space Administration ;, 1972), by Gary L. Giles, Melvin S. Anderson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) Theoretical buckling loads of boron/aluminum and graphite/resin fiber-composite anisotropic plates (National Aeronautics and Space Administration ;, 1971), by C. C. Chamis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust) An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows (National Aeronautics and Space Administration ;, 1972), by Roop N. Gupta and Langley Research Center (page images at HathiTrust) NASA TN D-5467 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John E. Rohde, George W. Metger, Hadley T. Richards, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-3918 (National Aeronautics and Space Administration ;, 1967), by John G. Davis, George W. Zender, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Range of interface thermal conductance for aircraft joints (National Aeronautics and Space Administration, 1960), by Martin E. Barzelay and Syracuse University (page images at HathiTrust) Effect of iron behind beryllium in the Oak Ridge National Laboratory lid tank (expt. 38) (U.S. Atomic Energy Commission, Technical Information Service, 1955), by G. T. Chapman, J. D. Flynn, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust) NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Evan H. Schuette, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust) Experimental forces and free-surface elevations for a yawed surface-piercing plate (David W. Taylor Naval Ship Research and Development Center, 1977), by R. B. Chapman and David W. Taylor Naval Ship Research and Development Center (page images at HathiTrust) Eddy viscosities and mixing lengths for turbulent boundary layers on flat plates, smooth or rough (David W. Taylor Naval Ship Research and Development Center, 1986), by Paul S. Granville and David W. Taylor Naval Ship Research and Development Center (page images at HathiTrust) Evaluation of bearing plates installed on full-column resin-grouted bolts (U.S. Dept. of the Interior, Bureau of Mines, 1986), by Stephen C. Tadolini and Bryan F. Ulrich (page images at HathiTrust) Some experimental studies of panel flutter at Mach number 1.3 (National Advisory Committee for Aeronautics, 1952), by Maurice A. Sylvester, John E. Baker, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Preliminary results of stability calculations for the bending of box beams with longitudinally stiffened covers connected by posts (National Advisory Committee for Aeronautics, 1952), by Roger A. Anderson, Aldie E. Johnson, Wilder Thomas W., Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Preliminary investigations of strength characteristics of structural elements at elevated temperatures (National Advisory Committee for Aeronautics, 1953), by Eldon E. Mathauser, Charles Libove, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) A study of the response of panels to random acoustic excitation (National Advisory Committee for Aeronautics, 1955), by R. W. Hess, Harvey H. Hubbard, Leslie W. Lassiter, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Experimental and theoretical studies of panel flutter at Mach number 1.2 to 3.0 (National Advisory Committee for Aeronautics, 1955), by Maurice A. Sylvester, Herbert J. Cunningham, Herbert C. Nelson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Laminar flow of a slightly viscous incompressible fluid that issues from a slit and passes over a flat plate (National Advisory Committee for Aeronautics, 1948), by Neal Tetervin and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Analysis of turbulent free-convection boundary layer on flat plate (National Advisory Committee for Aeronautics, 1950), by E. R. G. Eckert, Thomas W. Jackson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Deflection and stress analysis of thin solid wings of arbitrary plan form with particular reference to delta wings (National Advisory Committee for Aeronautics, 1952), by Manuel Stein, John M. Hedgepath, J. Edward Anderson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) The hydrodynamic characteristics of an aspect-ratio-0.125 modified rectangular flat plate operating near a free water surface (National Advisory Committee for Aeronautics, 1954), by John A. Ramsen, Victor L. Vaughan, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Experimental and theoretical determination of thermal stresses in a flat plate (National Advisory Committee for Aeronautics, 1952), by Richard R. Heldenfels, William M. Roberts, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Collision of plates (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Division of Technical Information, 1953., 1953), by H. Poritsky, M.F. Bolster, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust) Three low-pressure spall thresholds in copper (Sandia Corporation, 1963), by J. H. Smith, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust) On the stability of stiffened plates (U.S. Experimental Model Basin, Navy Yard, 1935), by Stephen Timoshenko, Dwight F. Windenburg, M.C. Roemer, and U.S. Experimental Model Basin (page images at HathiTrust) The Effect of an arbitrary surface-temperature variation along a flat plate on the convective heat transfer in an incompressible turbulent boundary layer (National Advisory Committee for Aeronautics, 1951), by Morris W. Rubesin and United States National Advisory Committee for Aeronautics (page images at HathiTrust) An Experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow (National Advisory Committee for Aeronautics, 1951), by Robert W. Higgins, Constantine C. Pappas, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Heat, mass, and momentum transfer for flow over a flat plate with blowing or suction (National Advisory Committee for Aeronautics, 1954), by H. S. Mickley and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Impulsive loading of a circular disk (Sandia Corporation ;, 1961), by W. B. Murfin and Sandia Corporation (page images at HathiTrust) NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), by H. Page Hoggard, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1944), by Paul Kuhn, L. Ross Levin, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), by Merven W. Mandel, Evan H. Schuette, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Stresses and displacements in perforated plates (Purdue University, 1964), by John Edward Goldberg and K. N. Jabbour (page images at HathiTrust) Thermal stresses in perforated plates (Schenectady, New York : Knolls Atomic Power Laboratory, 1951., 1951), by G. Horvay, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust) Bending of honeycombs and of perforated plates (Schenectady, New York : Knolls Atomic Power Laboratory, 1952., 1952), by G. Horvay, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust) Philosophy of structural response to normal and abnormal loads. (U.S. Office of Policy Development and Research, Dept. of Housing and Urban Development, 1976), by United States. Dept. of Housing and Urban Development. Office of Policy Development and Research (page images at HathiTrust) Fabrication of UO2-stainless steel dispersion fuel for BORAX-V nuclear superheat (Argonne National Laboratory, Metallurgy Division, 1963), by W. C. Kramer, C. H. Bean, and Argonne National Laboratory (page images at HathiTrust) Irradiation of an aluminum alloy-clad ceramic pellet-fueled plate (Argonne National Laboratory, Reactor Engineering Division, 1960), by A. P. Gavin and Argonne National Laboratory (page images at HathiTrust) Bending of circular plates under a variable symmetrical load (Argonne National Laboratory, Particle Accelerator Division, 1964), by J. C. Heap and Argonne National Laboratory (page images at HathiTrust) Bending of circular plates under a uniform load on a concentric circle (Argonne National Laboratory, Particle Accelerator Division, 1964), by J. C. Heap and Argonne National Laboratory (page images at HathiTrust) Bending of honeycombs and of perforated plates (Schenectady, New York : Knolls Atomic Power Laboratory, 1952., 1952), by G. Horvay, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust) On the Steady-state thermoelastic problem for the half-space and the thick plate ([United States Air Force, Office of Scientific Research], 1959), by Ian Naismith Sneddon, F. J. Lockett, United States. Air Force. Office of Scientific Research, and Duke University (page images at HathiTrust) Stress in the vicinity of a crack in a thick elastic plate (Washington D. C. : Mathematics Division, Office of Scientific Research, U.S. Air Force, 1960., 1960), by Morton Lowengrub, United States. Air Force. Office of Scientific Research, and Duke University (page images at HathiTrust) Thermal stresses in perforated plates (Schenectady, New York : General Electric Company, Knolls Atomic Power Laboratory, 1951., 1951), by G. Horvay, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust) On stress interaction in fatigue and cumulative damage rule : part II. 7075 aluminum alloy (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1960., 1956), by Alfred M. Freudenthal, Robert A. Heller, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust) Supersonic panel flutter (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1957., 1957), by Yudell L. Luke, Andrew St. John, United States. Air Force. Air Research and Development Command, Midwest Research Institute, and Wright Air Development Center (page images at HathiTrust) A wind tunnel investigation of jets exhausting into a crossflow. Volume III, Additional data for two-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust) A wind tunnel investigation of jets exhausting into a crossflow. Volume 2, Additional data for the one-jet configuration (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust) Large amplitude response of complex structures due to high intensity noise (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), by C. Mei, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust) Investigation of weldability of hot-work tool steels (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by N. A. Sinclair, R. P. Sopher, J. G. Maciora, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and General Dynamics Corporation. Electric Boat Division (page images at HathiTrust) A wind tunnel investigation of jets exhausting into a crossflow. Volume 4, Additional data for three-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust) Viscoelastic support damping of built-in circular plates (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by T. J. Mentel, R. L. Schultz, University of Minnesota, Air Force Materials Laboratory (U.S.), Wright-Patterson Air Force Base (Ohio), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust) NASTRAN stress recovery package (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), by Steven E. Lamberson, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust) Analyses of elasto-plastic plates with cracks (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by J. L. Swedlow, W. Yang, M. L. Williams, Air Force Materials Laboratory (U+.S.), and California Institute of Technology (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) Investigation of the distribution of tensile and bending stresses in notched flat bars (Wright-Patterson Air Force Base, Ohio : AF Materials Laboratory, Aeronautical Systems Division, Air Force Systems Command, 1963., 1963), by Heinz Neuber, United States. Air Force. Systems Command. Aeronautical Systems Division, Technische Hochschule München, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust) Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 2, Summary of test data (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by P. C. Huang, 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) Response of nonlinear structural panels subjected to high intensity noise (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by C. Mei, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Missouri--Rolla. Mechanical Engineering Department (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) An application of the finite element method to elastic-plastic problems of plane stress (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by M. Salmon, R. Sandhu, L. Berke, Air Force Flight Dynamics Laboratory (U.S.), and IIT Research Institute (page images at HathiTrust) A wind tunnel investigation of jets exhausting into a crossflow. Volume 1, Test description and data analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust) Design development and durability validation of postbuckled composite and metal panels: technology assessment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), by Ravi B. Deo, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust) Anisotropic plates. ([Office of Technical Services, U.S. Dept. of Commerce], 1967), by S. G. Lekhnit︠s︡kiĭ and United States. Department of Commerce. Office of Technical Services (page images at HathiTrust) Stress and strain distribution in the vicinity of interference fit fasteners (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Merle Allen, J. A. Ellis, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Convair Division (page images at HathiTrust) Creep behavior of structural insulated panels (SIPs) : results from a pilot study (Madison, WI. : United States Department of Agriculture, Forest Service, Forest Products Laboratory, 2014., 2014), by Dwight McDonald and Forest Products Laboratory (U.S.) (page images at HathiTrust)
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