The Online Books Page

Cylinders

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

• Aluminum cylinders
• Gas cylinders
• Pressurized cylinders

• Effects of sting-support interference on the drag of an ogive-cylinder body with and without a boattail at 0.6 to 1.4 mach number / (Washington : National Advisory Committee for Aeronautics, [1957]), by George Lee, James L. Summers, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Application of multivariable search techniques to structural design optimization / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Robert T. Jones, D. S. Hague, Langley Research Center, and Aerophysics Research Corporation (page images at HathiTrust)
• Preliminary results of compression tests on cylinders with eccentric longitudinal stiffeners / (Washington, D.C. : National Aeronautics and Space Administration ; Washington, D.C. : For sale by the Office of Technical Services, Department of Commerce [distributor], 1964), by Michael F. Card and Langley Research Center (page images at HathiTrust)
• Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by William L. Wells and Langley Research Center (page images at HathiTrust)
• Finite-amplitude pressure waves in the radial mode of a cylinder / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Isoroku Kubo, F. K. Moore, Lewis Research Center, and Cornell University (page images at HathiTrust)
• Subsonic sting interference on the aerodynamic characteristics of a family of slanted-base ogive-cylinders / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Colin P. Britcher, W. Allen Kilgore, Charles W. Alcorn, Langley Research Center, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics (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)
• Boundary layer stability on a yawed spinning body of revolution and its effect on the magnus force and moment / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by I. D. Jacobson, J. B. Morton, Langley Research Center, and University of Virginia (page images at HathiTrust)
• An integral-equation solution for TE radiation and scattering from conducting cylinders / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by J. H. Richmond, Langley Research Center, and Ohio State University (page images at HathiTrust)
• An investigation of the vibration characteristics of pressurized thin-walled circular cylinders partly filled with liquid / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1962), by John S. Mixson, Robert W. Herr, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Buckling tests of two integrally stiffened cylinders subjected to bending / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by James Kent Anderson, James P. Peterson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Influence of edge conditions on the stability of axially compressed cylindrical shells / ([Washington] : National Aeronautics and Space Administration, [1965]), by B. O. Almroth, Lockheed Missiles and Space Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical and experimental studies of the natural convection within a horizontal cylinder / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Roger B. Stewart, Lillian R. Boney, Alexander P. Sabol, and Langley Research Center (page images at HathiTrust)
• Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Milton Lamb, Robert L. Stallings, and Langley Research Center (page images at HathiTrust)
• Kinematic stability of roller pairs in free-rolling contact / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1976), by M. Savage, Stuart H. Loewenthal, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Transient viscous flow around an elliptic cylinder / (Urbana, Illinois : Dept. of Computer Science, University of Illinois at Urbana-Champaign, 1974), by Gary Arthur Roediger (page images at HathiTrust)
• A new method of analyzing the cylinder performance of reciprocating engines / (1911), by Jean Paul Clayton (page images at HathiTrust; US access only)
• Experimental study of the effectiveness of cylindrical plume simulators for predicting jet-on boattail drag at Mach numberes up to 1.30 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by David E. Reubush and Lanlgely Research Center (page images at HathiTrust)
• Thermal stresses and strains in a finite cylinder with no surface forces / (Oak Ridge, Tenn. : U.S. Atomic Energy Commission. Technical Information Division, 1951), by F. H. Murray, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Surface roughness effects on the mean flow past circular cylinders / (Iowa City : Institute of Hydraulic Research, University of Iowa, 1975), by Oktay Güven, V. C. Patel, and National Science Foundation (U.S.) (page images at HathiTrust; US access only)
• Diffraction by a perfectly conducting rectangular cylinder which is illuminated by an array of line sources / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1974]), by R. G. Kouyoumjian, N. Wang, Langley Research Center, and Ohio State University. ElectroScience Laboratory (page images at HathiTrust)
• The stabilizing effectiveness of conical flares on bodies with conical noses / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Donn B. Kirk, Gary T. Chapman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders / (Washington, D.C. : National Advisory Committee for Aeronautics, 1934), by Oscar W. Schey, Vern G. Rollin, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Library (page images at HathiTrust)
• Partially plastic thick-walled cylinders. A portion of a research project entitled plastic behavior of engineering materials. (Urbana, Dept. of Theoretical and Applied Mechanics, University of Illinois., 1952), by Montogomerie Christie Steele (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)
• Aerodynamic forces on a stationary and oscillating circular cylinder at high Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969), by George W. Jones, Robert W. Walker, Joseph J. Cincotta, George C. Marshall Space Flight Center, Martin Company, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effects of surface and through cracks on failure of pressurized thin-walled cylinders of 2014-T6 aluminum / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by William S. Pierce, Lewis Research Center, and United States National Aeronautics and Space Administration (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)
• Surface heat-transfer coefficients of pin-finned cylinders / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by G. James VanFossen, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Randall C. Davis, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Heat-transfer measurements on a low-fineness-ratio cylinder at a mach number of 10.4 and angles of attack from 0° to 90° / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Philip E. Everhart and Langley Research Center (page images at HathiTrust)
• Certain bimetallic cylinders from Japan : determination of the Commission in investigation no. 731-TA-383(preliminary) under the Tariff act of 1930, together with the information obtained in the investigation. (Washington, D.C. : U.S. International Trade Commission, 1987), by United States International Trade Commission (page images at HathiTrust)
• Certain bimetallic cylinders from Japan : determination of the Commission in investigation no. 731-TA-383 (final) under the Tariff act of 1930, together with the information obtained in the investigation. (Washington, D.C. : U.S. International Trade Commission, 1988), by United States International Trade Commission (page images at HathiTrust)
• Experimental aerodynamic characteristics for a cylindrical body of revolution with various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
• Experimental aerodynamic characteristics for a cylindrical body of revolution with side strakes and various noses at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Leland H. Jorgensen, Edgar R. Nelson, and Ames Research Center (page images at HathiTrust)
• The pressure and deformation profile between two colliding lubricated cylinders / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Kwan Moh Lee, H. S. Cheng, Lewis Research Center, and Ill.) Northwestern University (Evanston (page images at HathiTrust)
• Numerical calculations of viscous compressible fluid flow around a stationary cylinder / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by John G. Trulio, Leonard Walitt, George C. Marshall Space Flight Center, and inc Applied Theory (page images at HathiTrust)
• Numerical calculation of viscous compressible fluid flow around an oscillating rigid cylinder / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by John G. Trulio, Leonard Walitt, George C. Marshall Space Flight Center, and inc Applied Theory (page images at HathiTrust)
• Design and fabrication of a ring-stiffened graphite-epoxy corrugated cylindrical shell / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Read Johnson, McDonnell Douglas Astronautics Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Heat transfer to cylinders in crossflow in hypersonic rarefied gas streams / (Washington : National Aeronautics and Space Administration, [1960]), by Ruth N. Weltmann, Perry W. Kuhns, and Lewis Research Center (page images at HathiTrust)
• Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/ (Washington : National Aeronautics and Space Administration, [1962]), by Lovick O. Hayman, Russell W. McDearmon, and Langley Research Center (page images at HathiTrust)
• Structural behavior and compressive strength of circular cylinders with longitudinal stiffening / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 19]), by James P. Peterson, Jerry W. Deaton, Ralph O. Whitley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of Reynolds number and flow incidence on the force characteristics of a family of flat-front cylinders / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Vernard E. Lockwood, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Interference heating on a swept cylinder in region of intersection with a wedge at Mach number 8 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Dennis M. Bushnell and Langley Research Center (page images at HathiTrust)
• Flow visualization of discrete-hole film cooling with a spanwise injection over a cylinder / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Louis M. Russell, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Structural efficiency of ring-stiffened corrugated cylinders in axial compression / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by James P. Peterson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Configuration factors for exchange of radiant energy between axisymmetrical sections of cylinders, cones, and hemispheres and their bases / (Washington : National Aeronautics and Space Administration, [1961]), by Albert J. Buschman, C. M. Pittman, and Langley Research Center (page images at HathiTrust)
• Elastoplastic analysis of circular cylindrical inclusion in uniformly stressed infinite homogeneous matrix / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1968]), by Alexander Mendelson 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)
• Predictive equations for thermal neutron flux perturbation effects in cylinders / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by John H. Lynch, Lawrence E. Peters, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Shock-tube heat-transfer measurements on inner surface of a cylinder (simulating a flat plate) for stagnation-temperature range 4,100 ̊to 8,300 ̊R / (Washington : National Aeronautics and Space Administration, [1959]), by Jim J. Jones and Langley Research Center (page images at HathiTrust)
• Laminar boundary-layer separation induced by flares on cylinders with highly cooled boundary layers at a Mach number of 15 / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1965]), by Donald M. Kuehn and Ames Research Center (page images at HathiTrust)
• Mixing of wakes in a turbulent shear flow / (Washington : National Aeronautics and Space Administration, [1959]), by Salamon Eskinazi and Syracuse University (page images at HathiTrust)
• Local heat-transfer characteristics of a row of circular air jets impinging on a concave semicylindrical surface / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by John N. B. Livingood, James W. Gauntner, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Irving Weinstein, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Boundary layer measurements in an accelerated flow with and without heat transfer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Howard L. Wesoky, Charlene May, and Lewis Research Center (page images at HathiTrust)
• Experimental profiles of velocity components and radial pressure distributions in a vortex contained in a short cylindrical chamber / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1965), by Joseph M. Savino, Edward G. Keshock, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• The general instability of ring-stiffened corrugated cylinders under axial compression / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by John N. Dickson, Richard H. Brolliar, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Snap-through and post-buckling behavior of cylindrical shells under the action of external pressure, (Urbana, 1957]), by Henry L. Langhaar and Arthur P. Boresi (page images at HathiTrust; US access only)
• 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)
• Buckling of imperfect cylinders under axial compression / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by G. A. Thurston and M. A. Freeland (page images at HathiTrust; US access only)
• Buckling of cylindrical shell end closures by internal pressure / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by G. A. Thurston and A. A. Holston (page images at HathiTrust; US access only)
• The influence of the boundary conditions on the buckling load of cylindrical shells under axial compression / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Shigeo Kobayashi (page images at HathiTrust; US access only)
• 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)
• Viscous flow in a short cylindrical vortex chamber with a finite swirl ratio / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Robert W. Hornbeck, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect of roughness on heat transfer to hemisphere cylinders at Mach numbers 10.4 and 11.4 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1967), by James C. Dunavant, Howard W. Stone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect of end condition of cylinder on compressive strength of concrete, ([Chicago] Structural materials research laboratory, 1925), by Harrison F. Gonnerman (page images at HathiTrust)
• The effect of a rotating cylinder at the leading and trailing edges of a hydrofoil / (China Lake, Calif. : U.S. Naval Ordnance Test Station, [1963]), by John D Brooks and Calif.) Naval Ordnance Test Station (China Lake (page images at HathiTrust; US access only)
• Influence of ring stiffeners on instability of orthotropic cylinders in axial compression / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1964), by David L. Block, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect of residual stress on fracture strength of AISI 301 stainless-steel and Ti-5A1-2.5Sn eli titanium cracked thin-wall cylinders / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Frederick D. Calfo and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Mechanical behavior of boron-epoxy and glass-epoxy filament-wound cylinders under various loads, ([Washington] National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1969]), by Harvey W. Herring, Richard A. Pride, and Robert M. Baucom (page images at HathiTrust; US access only)
• Natural convection heating and cooling by horizontal cylinders : final report / (New York, NY : Columbia University, 1953), by Charles F. Bonilla, J. P. Collins, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Location of separation on a circular cylinder in crossflow as a function of Reynolds Number / (Bethesda, Md. : Naval Ship Research and Development Center, [1971]), by David W. Coder and Naval Ship Research and Development Center (page images at HathiTrust)
• Waste minimization assessment for a manufacturer of rotogravure printing cylinders / (Cincinnati, OH : U.S. Environmental Protection Agency, Risk Reduction Engineering Laboratory, [1993]), by Marvin Fleischman, Gwen P. Looby, F. William Kirsch, and Risk Reduction Engineering Laboratory (U.S.) (page images at HathiTrust)
• Air and oil cylinders in industrial applications. (Cleveland, Applied hydraulics magazine, Industrial Pub. Group, 1954), by Elmer F. Heiser (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)
• Testing of ten-ton uranium hexafluoride cylinders /, by W. R. Pedigo, J. L. Myers, W. J. Hamer, S. Bernstein, V. A. Smith, sponsor Carbide and Carbon Chemicals Corporation, issuing body Union Carbide Nuclear Company, and sponsor U.S. Atomic Energy Commission (page images at HathiTrust)
• Distortion of a magnetic field by the motion of a cylindrical conductor /, by Joseph G. Kelley, Ronald S. Finn, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Second report of the Gas cylinders research committee (Periodical heat treatment). (London, H. M. Stationery off. [printed by Harrison and sons, ltd.], 1926), by Great Britain. Dept. of scientific and industrial research. Gas cylinders research committee and Henry Cort Harold Carpenter (page images at HathiTrust)
• Air forces on circular cylinders, axes normal to the wind, with special reference to dynamical similarity / ([Washington, D.C. : U.S. Dept. of Commerce, Bureau of Standards : U.S. Govt. Print. Off., 1920]), by Hugh L. Dryden and United States. National Bureau of Standards. Scientific Papers (page images at HathiTrust)
• Temperature and stress formulae for cylinders with heat generated in the material / (Oak Ridge, Tenn. : U.S. Atomic Energy Commission, Technical Information Service, 1953), by C. F. Leyse, Phillips Petroleum Company. Atomic Energy Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The fabrication of hollow hemispheres and cylinders of tungsten carbide-6 w/o cobalt / (Los Alamos, N.M. : Los Alamos Scientific Laboratory of the University of California, 1964), by Haskell Sheinberg, T. L. Herrera, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Temperature profiles within cylinders containing internal heat sources and materials of temperature-dependent thermal conductivities : description of fast computer programs as applied to solidified radioactive wastes / (Oak Ridge, Tenn. : Oak Ridge National Laboratory, 1969), by W. Davis, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Critical stress of ring-stiffened cylinders in torsion / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Manuel Stein, Harold Crate, J. Lyell Sanders, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Temperature distribution in a metal cylinder containing a heat source / (Oak Ridge, Tenn. : United States Atomic Energy Commission, Technical Information Service, 1953), by Leon Pletke, Glenn H. Murphy, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Temperature distribution in a cylindrical solid with symmetrically-placed longitudinal coolant channels / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation, [1961]), by J. F. Heyda, R. C. Herrmann, General Electric Company. Nuclear Materials and Propulsion Operation, United States Air Force, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effects of dissolved gas evolution at the surfaces of heated vertical cylinders /, by Jerry R. Peterson and U.S. Atomic Energy Commission (page images at HathiTrust)
• Axial loading of a cylindrical container /, by D. P. Timo, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Self-shielding factors for infinitely long, hollow cylinders /, by J. Dwork, E. F. Clancy, H. Hurwitz, P. L. Hofmann, U.S. Atomic Energy Commission, General Electric Company, and Knolls Atomic Power Laboratory (page images at HathiTrust)
• Drag of several surface protrusion patterns at M = 5.0 /, by John A. Darling and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Thermal stresses and strains in a finite cylinder with no surface forces / (Oak Ridge, Tenn., U.S. Atomic Energy Commission. Technical Information Division, 1945), by F. H. Murray, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Experiments on copper crusher cylinders / (Washington, D.C. : U.S. Dept. of Commerce, Bureau of Standards : U.S. Govt. Print. Off., 1921), by Alexander I. Krynitsky and United States. National Bureau of Standards. Technologic Papers (page images at HathiTrust)
• Elastic constants and sound velocities. (Oak Ridge, Tenn. : U.S. Atomic Energy Commission, Technical Information Division, ORE, [1950]), by Myra F. Kilpatrick, John E. Kilpatrick, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Curie evaluation of hollow cylinder sources / (Upton, N.Y. : Brookhaven National Laboratory, 1953), by Otto A. Kuhl, Walter Rosenzweig, Bernard Manowitz, U.S. Atomic Energy Commission, and Brookhaven National Laboratory (page images at HathiTrust)
• Maximum temperature rise in cylinders containing intermediate-level and high-level solidified radioactive wastes / (Oak Ridge, Tenn. : Oak Ridge National Laboratory, 1969), by W. Davis, H. F. Soard, C. L. Fitzgerald, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Preliminary investigation of the failure of pressurized stiffened cylinders / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Norris F. Dow, Roger W. Peters, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Charles B. Rumsey, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The thermal fracture of ceramic cylinders / (Columbus, OH : Battelle Memorial Institute, [1956]), by Winston H. Duckworth, Eugene M. Simons, Eugene Michael Baroody, Allison K. Smalley, U.S. Atomic Energy Commission, and Battelle Memorial Institute (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 / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1947), by Louis G. Dunn and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Stresses in and general instability of monocoque cylinders with cutouts. 7- Experimental investigation of cylinders having either long bottom cutouts or series of side cutouts / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Nicholas J. Hoff, Joseph J. Mele, Bruno A. Boley, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transverse vibrations of hollow thin-walled cylindrical beams / (Washington D. C. : National Advisory Committee for Aeronautics, 1952), by Bernard Budiansky, Edwin T. Kruszewski, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of variable viscosity and thermal conductivity on high-speed slip flow between concentric cylinders / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by T. C. Lin, R. E. Street, 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Harvey G. McComb and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Summary of drag coefficients of various shaped cylinders / (Cincinnati, Ohio : General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, Technical Publications Sub-Section ; Washington, D.C. : Available from the Office of Technical Services, U.S. Dept. of Commerce, 1957), by C. F. Heddleson, General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Structural analysis of the ANP concentric ring fuel element / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation, 1961), by D. R. Riley, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Supersonic drag and base pressure of a 70©� cone cylinder /, by George D. Kahl, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Some experiments with liquid-filled, impulsively started, spinning cylinder /, by Gene Sokol and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Ultrasonic inspection of bonded cylinders /, by H. E. VanValkenburg, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Additional testing of ten-ton uranium hexafluoride cylinders /, by E. W. Richardson, S. Bernstein, Carbide and Carbon Chemicals Corporation, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Testing of fourteen-ton uranium hexafluoride cylinders /, by E. W. Richardson, S. Bernstein, V. A. Smith, Union Carbide Corporation. Nuclear Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The calculation of thermal stress in cylinders with internal heat generation /, by Duane M Davis, Benjamin H. Mount, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (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)
• Mathematical analysis of heat conduction in a sector of a hollow circular cylinder /, by Martin Company and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Heat transfer on an afterbody immersed in the separated wake of a hemisphere / (Washington, D.C. : National Advisory Committee for Aeronautics, [1958]), by Helmer V. Nielsen, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by Earl D. Knechtel, Arvid N. Andrea, Ames Research Center, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of method of preparation of ends of concrete cylinders for testing / (Vicksburg, Miss. : Waterways Experiment Station, 1972), by K. L. Saucier, Waterways Experiment Station (U.S.), and United States Army Corps of Engineers (page images at HathiTrust)
• The elastic response of buried cylinders : critical literature review and pilot study / (Vicksburg, Miss. : Waterways Experiment Station, 1966), by Gayle E. Albritton, Waterways Experiment Station (U.S.), and United States. Defense Atomic Support Agency (page images at HathiTrust)
• Critical geometries for bare cylinders / (Portsmouth, Ohio : Goodyear Atomic Corporation ; Washington, D.C. : Available from the Office of Technical Services, U.S. Dept. of Commerce ;, 1956), by J. A. Pond, Goodyear Atomic Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust; US access only)
• Fundamental studies of medium-structure interaction : report 1 : finite element analysis of buried cylinders / (Vicksburg, Miss. : Waterways Experiment Station, 1972), by Jesse L. Kirkland and Robert E. Walker (page images at HathiTrust)
• Behavior of stiff cylinders buried in sand under static loading / (Vicksburg, Miss. : Waterways Experiment Station, 1973), by Charles D. Norman and J. D. Prendergast (page images at HathiTrust)
• Static loading of shallow-buried model cylinders : Phase II of III : final report / (Vicksburg, Mississippi : Waterways Experiment Station, 1978), by Van T. Cost, James M. Watt, Space and Missile Systems Organization (U.S.), and United States. Defense Nuclear Agency (page images at HathiTrust)
• Heat transfer by natural convestion from horizontal cylinders to liquid metals : final report for July 1, 1949 to June 30, 1950 /, by Seymour C. Hyman, Charles F. Bonilla, Columbia University, and U.S. Atomic Energy Commission. New York Operations Office (page images at HathiTrust)
• Natural convection transfer processes, by Seymour C. Hyman, Stanley W. Ehrlich, Charles F. Bonilla, Columbia University, and U.S. Atomic Energy Commission. New York Operations Office (page images at HathiTrust)
• Strength tests on paper cylinders in compression, bending, and shear / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1931), by Richard V. Rhode, Eugene E. Lundquist, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A Numerical approach to the instability problem of monocoque cylinders / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Bruno A. Boley, Mayers. J., Josesph Kempner, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Torsional vibrations of hollow thin-walled cylindrical beams / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Edwin T. Kruszewski, Eldon E. Kordes, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Welding thin-walled uranium cylinders : a monograph /, by E. L. Brundige and U.S. Atomic Energy Commission (page images at HathiTrust)
• Instability phenomena in thin-walled cylinders /, by W. R. Russ, Frederick Forscher, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Flux from homogeneous cylinders containing uniform source distributions /, by J. J. Taylor, F. E. Obenshain, Westinghouse Electric Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Response of horizontally oriented buried cylinders to static and dynamic loading / (Vicksburg, Miss. : Waterways Experiment Station, 1965), by Albert F. Dorris (page images at HathiTrust)
• Field investigation of a neoprene pad capping system / ([Vicksburg, Miss. : U.S. Army Engineer Waterways Experiment Station] ; [Springfield, Va.] : [Available from National Technical Information Service], [1988]), by Billy D. Neeley, Robert J. Becker, United States Army Corps of Engineers, and U.S. Army Engineer Waterways Experiment Station (page images at HathiTrust)
• Elastic response of shock-isolated cylinders buried in a dense, dry sand / (Vicksburg, Miss. : Waterways Experiment Station, 1969), by David C. Foster and United States. Defense Atomic Support Agency (page images at HathiTrust)
• Minimum critical cylinder diameters of hydrogen moderated U(4.9) systems / (Oak Ridge, Tenn. : Union Carbide Corporation, Nuclear Division, 1965), by C. E. Newlon, Union Carbide Corporation. Nuclear Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The shearing rigidity of curved panels under compression / (Washington, D.C. : National Advisory Committee for Aeronautics, 1946), by Nicholas J. Hoff, Bruno A. Boley, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of compressibility at high subsonic velocities on the lifting force acting on an elliptic cylinder / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1946), by Carl Kaplan and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Stress analysis of circular semimonocoque cylinders with cutouts by a perturbation load technique / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Harvey G. McComb and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Stresses in a semi-infinite thin-walled cylinder caused by an exponential temperature distribution /, by W. E. Cooper, J. L. Noble, M. T. Roche, U.S. Atomic Energy Commission, General Electric Company, and Knolls Atomic Power Laboratory (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)
• Finite deflection, discrete element analysis of shells /, by Fred K. Bogner, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Case Western Reserve University (page images at HathiTrust)
• Two dimensional analysis of transient heat conduction in a sector of a hollow circular cylinder /, by J. G. Torian, G. K. Bennett, sponsor Martin Company, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Inhibition of flow separation at high speed., by Jack Norman Nielsen, Frederick K. Goodwin, Larry L. Lynes, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Nielsen Engineering & Research (page images at HathiTrust)
• Tactual Coding of Cylindrical Knobs /, by James V. Bradley, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Creep and plastic deformation in cylindrical shells /, by Alfred M. Freudenthal, Maciej P. Bieniek, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor Columbia University (page images at HathiTrust)
• An investigation of separated flow about a hemisphere-cylinder at 0- to 19-deg incidence in the Mach number range from 0.6 to 1.5 /, by T. Hsieh, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Support interference on an ogive-cylinder model at high angle of attack in transonic flow /, by M. C. Altstatt, W. E. Dietz, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Numerical simulations and control of the flow past a circular cylinder /, by Mingqing Xiao, David B. Doman, Siva S. Banda, James H. Myatt, R. Chris Camphouse, Yuan Lin, sponsor Southern Illinois University at Carbondale. Department of Mathematics, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Aerodynamic characteristics of low aspect ratio fins at Mach numbers from 0.80 to 1.30 /, by D.K. Smith, R. C. German, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Aerodynamic characteristics of several low aspect ratio stabilizer fins at Mach numbers from 0.8 to 1.3 /, by J. M. Whoric, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Flow-field study about a hemisphere-cylinder in the transonic and low supersonic Mach number range /, by T. Hsieh, B. M. Majors, W. T. Strike, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• The Dynamics of spinning bodies at large angle of attack /, by J. E. Brunk, R. W. Rakestraw, W. L. Davidson, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 /, by W. T. Strike, S. Pate, Inc. sponsor ARO, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• Measurement of two-point correlations of velocity near a circular cylinder shedding a Karman Vortex street /, by Mahmoud Youssef el Baroudi, issuing body United States. Air Force. Office of Scientific Research, University of Toronto. Institute of Aerophysics, and sponsor University of Toronto. Institute of Aerophysics (page images at HathiTrust)
• Buckling of thin-walled cylinder under axial compression and internal pressure / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Hsu Lo, Edward B. Schwartz, Harold Crate, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)

More items available under narrower terms.