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Dead loads (Mechanics)

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• Loads (Mechanics)

• Loading, Static
• Static loads

• Statistical evaluation of the effectiveness of Federal Motor Vehicle Safety Standard 207: Seat Back Locks (Only). Final report. (1980), by John T. Ball, Gaylord M. Northrop, Jim C. Knoop, and E. Sweeton (page images at HathiTrust)
• Road simulator study of heavy-vehicle wheel forces. (1998), by D. A. Streit, Bohdan T. Kulakowski, P. E. Sebaaly, and R. J. Wollyung (page images at HathiTrust)
• Canopy and base load distribution on a longwall shield (U.S. Dept. of the Interior, Bureau of Mines, 1992), by Thomas M. Barczak, David F. Gearhart, and United States Bureau of Mines (page images at HathiTrust)
• Thermal-structural combined loads design criteria study (National Aeronautics and Space Administration ;, 1972), by V. Deriugin, Langley Research Center, and Boeing Company (page images at HathiTrust)
• NASA TN D-7002 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Sherwood Hoffman, Joseph J. Janos, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Static multiple-load measurement technique as utilized in the Naval Surface Weapons Center's wind tunnels (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1976., 1976), by John E. Holmes and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)

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

• 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)
• Structural optimization of sandwich and ring-stiffened 120 degree conical shells subjected to external pressure (National Aeronautics and Space Administration ;, 1969), by Gerald A. Cohen, Langley Research Center, and Philco-Ford Corporation (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)
• Structural behavior and compressive strength of circular cylinders with longitudinal stiffening (National Aeronautics and Space Administration :, 1962), by James P. Peterson, Jerry W. Deaton, Ralph O. Whitley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6351 (National Aeronautics and Space Administration ;, 1971), by Bernard J. Hamrock, David P. Fleming, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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)
• An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail (National Advisory Committee for Aeronautics, 1957), by Norman S. Land, Annie G. Fox, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing (National Advisory Committee for Aeronautics, 1958), by Edward C. Polhamus, Kenneth P. Spreemann, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some investigations of the general instability of stiffened metal cylinders. 9 - Criterions for the design of stiffened metal cylinders subject to general instability failures (National Advisory Committee for Aeronautics, 1947), by Louis G. Dunn and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip (National Advisory Committee for Aeronautics, 1949), by John D. Bird and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds (National Advisory Committee for Aeronautics, 1950), by John DeYoung and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions (National Advisory Committee for Aeronautics, 1950), by Richard R. Heldenfels and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lateral elastic instability of hat-section stringers under compressive load (National Advisory Committee for Aeronautics, 1951), by Stanley Goodman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• An Investigation of pure bending in the plastic range when loads are not parallel to a principal plane (National Advisory Committee for Aeronautics, 1951), by Harry A. Williams and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Bearing strengths of some aluminum-alloy permanent-mold castings (National Advisory Committee for Aeronautics, 1951), by E. M. Finley and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Fatigue testing machine for applying a sequence of loads of two amplitudes (National Advisory Committee for Aeronautics, 1951), by Richard Barksdale Harwell, Ira Smith, Darnley M. Howard, Frank C. Smith, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes (National Advisory Committee for Aeronautics, 1951), by Walter J. Klinar, Jack H. Wilson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings (National Advisory Committee for Aeronautics, 1952), by Franklin W. Diederich, Kenneth A. Foss, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theory and procedure for determining loads and motions in chine-immersed hydrodynamic impacts of prismatic bodies (National Advisory Committee for Aeronautics, 1952), by Emanuel Schnitzer, N. Grossman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A special investigation to develop a general method for thee-dimensional photoelastic stress analysis (National Advisory Committee for Aeronautics, 1952), by Max Mark Frocht, R. Guernsey, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow (National Advisory Committee for Aeronautics, 1953), by S. Katzoff, Hugh C. DuBose, M. Frances Faison, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of operating characteristics of four experimental and two conventional 75-millimeter-bore cylindrical-roller bearings at high speeds (National Advisory Committee for Aeronautics, 1953), by William J. Anderson, Zolton N. Nemeth, E. Fred Macks, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of bronze and nodular iron cage materials on cage slip and other performance characteristics of 75-millimeter-bore cylindrical-roller bearings at DN values of 2 X 10⁶. (National Advisory Committee for Aeronautics, 1953), by William J. Anderson, Zolton N. Nemeth, E. Fred Macks, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Stress distributions caused by three types of loading on a circular semimonocoque cylinder with flexible wings (National Advisory Committee for Aeronautics, 1954), by Harvey G. McComb and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The distribution of pressures through non-cohesive materials (1917), by Melvin Lorenius Enger (page images at HathiTrust; US access only)
• Collapse load of a spherical cap (Armour Research Foundation, Illinois Institute of Technology, 1959), by Philip Gibson Hodge, U.S. Atomic Energy Commission, and Armour Research Foundation (U.S.) (page images at HathiTrust; US access only)
• Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow (National Advisory Committee for Aeronautics, 1955), by M. J. Queijo and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of weights of 17ST and steel tubular structural members used in aircraft construction (National Advisory Committee for Aeronautics, 1931), by E. C. Hartmann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A Numerical approach to the instability problem of monocoque cylinders (National Advisory Committee for Aeronautics, 1951), by Bruno A. Boley, Mayers. J., Josesph Kempner, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• 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)
• Observations of the deformation of aluminum subjected to impulsive loads of constant maximum amplitude and variable impulse (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1960., 1960), by G. Moss, C. Glass, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• An X-ray analysis of the strain in steel due to impulsive loads (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1960., 1960), by G. Moss, C. Glass, S. Golaski, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45° sweptback wing at transonic speeds (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), by Donald D. Arabian, Charles F. Reid, Jack F. Runckel, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flat plates of plywood under uniform or concentrated loads (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1942), by Herman W. March, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Relation of strength of wood to duration of load (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1951), by L. W. Wood, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Preliminary evaluation of a vacuum-induced concentrated-load sandwich tester (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1952), by W. S. Ericksen, Bruce G. Heebink, Edward W. Kuenzi, University of Wisconsin, and Forest Products Laboratory (U.S.) (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)
• Effects of fighter attack spectrum on composite fatigue life (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by R. Badaliance, H. D. Dill, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• Automated method for the large deflection and instability analysis of three-dimensional truss and frame assemblies (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966), by R. H. Mallett, L. Berke, Case Institute of Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Elastic twist of straight wings (Wright-Patterson air force base, Dayton, Ohio : Air Documents Division, Intelligence Department, Headquarters, Air Materiel Command, 1948., 1948), by Walther Gustav Carl Boccius and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Loads acting on a ship (Experimental Towing Tank, Stevens Institute of Technology, 1957), by B. V. Korvin-Kroukovsky and Experimental Towing Tank (Laboratory) (page images at HathiTrust; US access only)
• Hydrodynamic forces (Experimental Towing Tank, Stevens Institute of Technology, 1958), by B. V. Korvin-Kroukovsky and Experimental Towing Tank (Laboratory) (page images at HathiTrust; US access only)
• In-flight measurements of captive loads on a store as compared with wind tunnel and mathematical simulations (China Lake, California : Naval Weapons Center, Aeromechanics Division, Systems Development Department, 1977., 1978), by A. R. Maddox, G. R. Mattasits, R. E. Dix, Inc ARO, United States. Air Force. Arnold Air Force Base, and Naval Weapons Center (page images at HathiTrust)
• Investigation of helicopter control loads induced by stall flutter (Fort Eustis, Virginia : U.S. Army Aviation Materiel Laboratories, 1970., 1970), by P. J. Arcidiacono, H. L. Elman, L. M. Casellini, F. O. Carta, U.S. Army Aviation Materiel Laboratories, and United Aircraft Corporation. Sikorsky Aircraft Division (page images at HathiTrust)
• Inviscid flow analysis on body of revolution with slender cruciform canted delta fins at small angle of incidence (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1975., 1975), by N. Uchiyama, J. M. Wu, Redstone Arsenal (Ala.), University of Tennessee (System). Space Institute, and Development United States. Army. Missile Command. Research (page images at HathiTrust)
• A method for computing rotary wing airload distribution iin forward flight (Fort Eustis, Virginia : U.S. Army Transportation Research Command, 1962., 1962), by Cornell Aeronautical Laboratory, Frank A. DuWaldt, Raymond A. Piziali, and United States. Army. Transportation Research Command (page images at HathiTrust)

More items available under broader and related terms at left.