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Damping (Mechanics)

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• A further study of the wave-damping properties of several geometric configurations of plastic material / ([Carderock, Md.] : Hydromechanics Laboratory, David Taylor Model Basin, [1960]), by Martha J Watts and David W. Taylor Model Basin. Hydromechanics Laboratory (page images at HathiTrust)
• Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Robert S. Swanson, E. LaVerne Priddy, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• The effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by John P. Campbell, John W. Paulson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Evaluation of an aeroelastic model technique for predicting airplane buffet loads [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1973), by Perry W. Hanson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ring-baffle pressure distribution and slosh damping in large cylindrical tanks / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Harland F. Scholl, Phillip K. Davis, David G. Stephens, and Langley Research Center (page images at HathiTrust)
• High performance, accelerometer-based control of the mini-MAST structure at Langley Research Center / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, VA : For sale by the National Technical Information Service, 1991), by Emmanuel G. Collins, Langley Research Center, and Harris Corporation. Government Aerospace Systems Division (page images at HathiTrust)
• Experimental investigation of the slosh-damping effectiveness of positive-expulsion bags and diaphragms in spherical tanks / (Washington : National Aeronautics and Space Administration, 1963), by Andrew J. Stofan and Irving E. Sumner (page images at HathiTrust)
• Friction and wear under fretting conditions of materials for use as wire friction dampers of compressor blade vibration / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Max A. Swikert, Robert L. Johnson, and Lewis Research Center (page images at HathiTrust)
• Design of an oil squeeze film damper bearing for a multimass flexible-rotor bearing system / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Robert E. Cunningham, David P. Fleming, Edgar J. Gunter, and Lewis Research Center (page images at HathiTrust)
• Subsonic roll-damping characteristics of a series of wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Richmond P. Boyden and Langley Research Center (page images at HathiTrust)
• Experimental evaluation of a tuned electromagnetic damper for vibration control of cryogenic turbopump rotors / (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 Eliseo DiRusso, Gerald V. Brown, and Lewis Research Center (page images at HathiTrust)
• Design and implementation of robust decentralized control laws for the ACES structure at Marshall Space Flight Center / (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 Emmanuel G. Collins, David C. Hyland, Douglas J. Phillips, Langley Research Center, and Harris Corporation. Government Aerospace Systems Division (page images at HathiTrust)
• Dynamics and stability of mechanical systems with follower forces / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by George Herrmann, United States. National Aeronautical and Space Administration, and Stanford University (page images at HathiTrust)
• Effect of support flexibility and damping on the dynamic response of a single mass flexible rotor in elastic bearings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by R. Gordon Kirk, Edgar J. Gunter, Lewis Research Center, and University of Virginia (page images at HathiTrust)
• Dynamic behavior of air lubricated pivoted-pad journal bearing - rotor system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970-1972), by Zolton N. Nemeth, William J. Anderson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Feasibility study and design of passive dampers for a manned rotating space station / ([Washington] : National Aeronautics and Space Administration, [1965]), by Engineering Mechanics Laboratory, TRW Space Technology Laboratories, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimentally determined stiffness and damping of an inherently compensated air squeeze-film damper / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Robert E. Cunningham and Lewis Research Center (page images at HathiTrust)
• Seismic retrofit of existing concrete frame structures using viscoelastic damping devices / ([Champaign, IL] : US Army Corps of Engineers, Construction Engineering Research Laboratory, 1995), by John R. Hayes and Construction Engineering Research Laboratory (page images at HathiTrust)
• Bibliography and tabulation of damping properties of non-metallic materials. (Wright-Patterson Air Force Base, Ohio, Directorate of Materials and Processes, Aeronautical Systems Division, 1962), by Sun Hwan Chi and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Bibliography of the material damping field (with abstracts and punched card codings) (Wright-Patterson Air Force Base, Ohio, Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1956), by L. J. Demer (page images at HathiTrust)
• Devices for damping mechanical vibrations, a bibliography. (Washington, Naval Research Laboratory, 1956), by Mildred Benton (page images at HathiTrust)
• Damping of flexural vibrations by alternate visco-elastic and elastic layers (Wright-Patterson Air Force Base, Ohio, Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1959 [i. e. 1960]), by Eric E. Ungar, Edward Michael Kerwin, and Donald Ross (page images at HathiTrust)
• Damping energy dissipation at support interfaces of square plates (Wright-Patterson Air Force Base, Ohio, Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1959), by Theodore Joseph Mentel and C. C. Fu (page images at HathiTrust)
• Damping energy dissipated by interfaces in beam and plate supports and in sandwich cores. (Wright-Patterson Air Force Base, Ohio, Wright Air-Patterson Center, Air Research and Development Command, U. S. Air Force, 1958 [i. e. 1959]), by Theodore Joseph Mentel (page images at HathiTrust)
• Response of bars (with internal and boundary damping) to transient and random excitation. (Wright-Patterson Air Force Base, Ohio, Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1959), by Robert F. Lambert (page images at HathiTrust)
• Dynamic soil-structure interaction / (Urbana, Ill. : Dept. of Civil Engineering, University of Illinois, [1980]), by Kuen-yaw Shye, A. R. Robinson, and University of Illinois at Urbana-Champaign. Dept. of Civil Engineering (page images at HathiTrust)
• Experimental and analytical investigation of the flutter of flat built-up panels under streamwise inplane load / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970), by R. W. Hess, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A study of damping in nonlinear oscillations / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by Maurice L. Rasmussen, Donn B. Kirk, Ames Research Center, Stanford University, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effects of vortex shedding on fuel slosh damping predictions / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Henry A. Cole, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect of material damping and stress distribution on the resonant fatigue strength of parts / (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1955), by Egons R. Podnieks, Benjamin Joseph Lazan, and United States. Wright Air Development Division (page images at HathiTrust)
• Damping behavior of dehavilland stem booms / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by R.E. Predmore, J.E. Jellison, C.L. Staugaitis, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of the damping contribution of an elastomeric ablator on aluminum beams / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by William E. Howell and Langley Research Center (page images at HathiTrust)
• Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Robert E. Cunningham and Lewis Research Center (page images at HathiTrust)
• Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by George W. Lewis, Roy D. Hager, and Lewis Research Center (page images at HathiTrust)
• Influence of oil-squeeze-film damping on steady-state response of flexible rotor operating to supercritical speeds / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Robert E. Cunningham and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Steady-state and transient analysis of a squeeze film damper bearing for rotor stability / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by L. E. Barrett, Edgar J. Gunter, Lewis Research Center, and University of Virginia (page images at HathiTrust)
• Predictions of F-111 TACT aircraft buffet response and correlations of fluctuating pressures measured on aluminum and steel models and the aircraft / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Charles F. Coe and Atlee M. Cunningham (page images at HathiTrust)
• Effects of control-response characteristics on the capability of a helicopter for use as a gun platform / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Robert J. Pegg, Andrew B. Connor, and Langley Research Center (page images at HathiTrust)
• Experimental investigation of the effect of model scale on structural-joint damping / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by David G. Stephens, Maurice A. Scavullo, Brantley R. Hanks, and Langley Research Center (page images at HathiTrust)
• Damping in tapered annular seals for an incompressible fluid / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by David P. Fleming, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Mechanical design handbook for elastomers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), by M. Darlow, E. Zorzi, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An experimental investigation of the viscous damping of liquid sloshing in spherical tanks / (Washington, D.C. : National Aeronautics and Space Administration, [1963]), by Irving E. Sumner, Andrew J. Stofan, and Lewis Research Center (page images at HathiTrust)
• Vibration of shaft face seals and stabilizing effect of viscous and friction damping / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Thomas N. Strom, John C. Hudelson, Lawrence P. Ludwig, and Lewis Research Center (page images at HathiTrust)
• Damping of a torsional oscillator in liquid helium 4 and 3 from 0.4 ̊to 2.5 ̊K / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Rayjor W. H. Webeler, David C. Hammer, and Lewis Research Center (page images at HathiTrust)
• Analytical comparison of effects of solid-friction and viscous structural damping on panel flutter / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Herbert J. Cunningham and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of wall roughness on the damping of liquid oscillations in rectangular tanks / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Frank M. Bugg, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static and dynamic stability derivatives of a model of a jet transport equipped with external-flow jet-augmented flaps / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by Delma C. Freeman, Richard D'Amato, Sue B. Grafton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some limitations on the use of damping in short pressure probes / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Ted W. Nyland, Robert C. Anderson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of structural response with different forms of damping / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by R. R. Reed and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of structural damping on flutter of stressed panels / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Charles P. Shore, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Experimental investigation of flutter at Mach 3 of rotationally restrained panels and comparison with theory / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Charles P. Shore, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Use of aircraft for zero-gravity environment / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by James W. Useller, Fred W. Haise, John N. Enders, Flight Research Center (U.S.), Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Moment of inertia and damping of liquids in baffled cylindrical tanks / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Franklin T. Dodge and Daniel D. Kana (page images at HathiTrust; US access only)
• A comparison of theoretical and experimental pressures and forces acting on a ring baffle under sloshing conditions / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Luis R. Garza (page images at HathiTrust; US access only)
• Conceptual design study for a mars entry vehicle damper / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by R. A. Winje (page images at HathiTrust; US access only)
• Vibration control (New York, McGraw-Hill, 1958), by John N. MacDuff and John R. Curreri (page images at HathiTrust)
• Technical manual operation and equipment instructions for in situ impulse test / (Washington, D.C. : The Division : Available from GPO Sales Program, Division of Technical Information and Document Control, U.S. Nuclear Regulatory Commission ; Springfield, Va. : National Technical Information Service, 1979), by Agbabian Associates, Shannon & Wilson, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Evaluation of in-situ soil damping characteristics / (Washington, D.C. : Division of Reactor Safety Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission ; GPO Sales Program, Division of Technical Information and Document Control, U.S. Nuclear Regulatory Commission ; Springfield, Va. : National Technical Information Service, 1980), by Agbabian Associates, Shannon & Wilson, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Photoelastic studies of damping, crack progagation and crack arrest in polymers and 4340 steel / (Washington, D.C. : The Commission : Available from GPO Sales Program, Division of Technical Information and Document Control, U.S. Nuclear Regulatory Commission ; Springfield, Va. : National Technical Information Service, 1980), by George Rankin Irwin, U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research, and College Park. Department of Mechanical Engineering University of Maryland (page images at HathiTrust)
• Pipe damping-results of vibration tests in the 33 to 100 hertz frequency range / (Washington, D.C. : Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1986), by Arthur G. Ware, Idaho National Engineering Laboratory, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology, and EG & G Idaho (page images at HathiTrust)
• Frictional damping and resonant vibration characteristics of an axial slip lap joint /, by James H. Klumpp, Benjamin J. Lazan, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Minnesota (page images at HathiTrust)
• Viscoelastic support junction damping of beams /, by Theodore Joseph Mentel, C. C. Fu, R. L. Schultz, sponsor United States. Air Force. Air Research and Development Command, and issuing body Wright Air Development Division (page images at HathiTrust)
• Damping of rectangular plate vibrations (Wright-Patterson Air Force Base, Ohio, Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1960), by Thomas S. Lundgren, Y. C. Whang, and Jieqian Zhang (page images at HathiTrust)
• A digital instrumentation package for an improved torsion pendulum / ([Avondale, Md.] : U.S. Dept. of the Interior, Bureau of Mines, 1983), by R. W. Nash and A. E. Schwaneke (page images at HathiTrust)
• Damping properties of selected steels and cast irons / ([Pittsburgh, Pa.] : U.S. Dept. of the Interior, Bureau of Mines, [1987]), by A. Visnapuu, P. C. Turner, and R. W. Nash (page images at HathiTrust)
• Pneumatic isolation systems with linear passive damping /, by D. B. DeBra, Richard E. Warner, and Lawrence Livermore Laboratory (page images at HathiTrust)
• Properties of manganese-copper alloys prepared from metal powders / ([Washington, D.C.] : Dept. of the Interior, Bureau of Mines, [1979]), by J. L. Holman, L. A. Neumeier, and R. L. Crosby (page images at HathiTrust)
• Damping capacity : its measurement and significance / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1959), by J. W. Jensen (page images at HathiTrust)
• Subsonic flight investigation of methods to improve the damping of lateral oscillations by means of a viscous damper in the rudder system in conjunction with adjusted hinge-moment parameters / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Harold L. Crane, John M. Elliott, George J. Hurt, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• A method of calculating a stability boundary that defines a region of satisfactory period-damping relationship of the oscillatory mode of motion / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Leonard Sternfield, Ordway B. Gates, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Ordway B. Gates, Albert A. Schy, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the law of damping of the luminescence of solid organic substances /, by V. A. Yastrebov, U.S. Atomic Energy Commission, and National Science Foundation (U.S.) (page images at HathiTrust)
• Motions of a payload on a tethered, aerodynamic-shape balloon using various cable lengths /, by Don E. Jackson, Catherine B. Rice, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Vibration isolation : use and characterization / (Washington : U.S. Dept. of Commerce, National Bureau of Standards, 1979), by John C. Snowdon and United States. National Bureau of Standards (page images at HathiTrust)
• A study of the rheological and damping properties of concrete / ([Urbana] : Dept. of Theoretical and Applied Mechanics, University of Illinois, 1960), by Mageed Girgrah, Clyde Ervin Kesler, and University of Illinois at Urbana-Champaign. Dept. of Theoretical and Applied Mechanics (page images at HathiTrust; US access only)
• Relationship between flutter parameters and generalized aerodynamic forces for wings of low aspect ratio /, by Bernard Mazelsky, Harry B. Amey, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Aerojet-General Corporation (page images at HathiTrust)
• Experiments on slip damping at rounded contacts /, by L. E. Goodman, C. B. Brown, sponsor United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command. issuing body, and sponsor University of Minnesota (page images at HathiTrust)
• Influence of damping in vibration isolation ([Washington]: Shock and Vibration Information Center, 1971), by Jerome E. Ruzicka, Thomas F. Derby, and Shock and Vibration Information Center (page images at HathiTrust; US access only)
• Pipe damping : experimental results from laboratory tests in the seismic frequency range / (Washington, D.C. : Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1986), by Arthur G. Ware, James G. Arendts, Idaho National Engineering Laboratory, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology, and EG & G Idaho (page images at HathiTrust)
• Damping capacity of soil during dynamic loading : report 1 : review of mathematical material models / (Vicksburg, Miss. : Waterways Experiment Station, 1972), by Behzad Rohani, Waterways Experiment Station (U.S.), and United States Army Corps of Engineers (page images at HathiTrust)
• Resonant column test / (Vicksburg, Miss. : U.S. Waterways Experiment Station ; Springfield, Va. : Available from National Technical Information Service, 1978), by Vincent P. Drnevich and Inc Soil Dynamics Instruments (page images at HathiTrust)
• A Study of the effects of damping on normal modes of electrical and mechanical systems., by Stephen F. Crumb, California Institute of Technology, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Evaluation of SDRC damping analysis / (Washington, D.C. : The Office ; Springfield, Va. : National Technical Information Service [distributor], 1980), by M. D. Noll, Structural Dynamics Research Corporation, and United States. Coast Guard. Office of Research and Development (page images at HathiTrust)
• Shock-wave attenuation properties of a bubble screen (U). (Vicksburg, Miss. : Waterways Experiment Station, 1961), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Measurements of growth and damping rates in an inhomogeneous low-beta plasma column /, by G. L. J. Mueller, R. S. Palmer, W. Friz, and issuing body Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• The damping of aluminum honeycomb sandwich beams /, by D. J. Mead, G. R. Froud, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor University of Southampton (page images at HathiTrust)
• A study to determine the effect of glass compositional variations on vibration damping properties /, by George A. Graves, B. Kumar, Charles Cannon, issuing agency Air Force Wright Aeronautical Laboratories, sponsor University of Dayton. Research Institute, and sponsor Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Beam vibrations with quasi-orthogonal boundary conditions /, by Y. C. Das, A. R. Robinson, Lawrence E. Goodman, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Analytical methods for determining specific damping energy considering stress distribution /, by E. R. Podnieks, B. J. Lazan, issuing body Wright Air Development Center, sponsor University of Minnesota, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Cable and piston drag parameter investigation for hydraulic aircraft-arresting energy absorbers /, by Howard L. Peterson, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and issuing agency United States. Air Force. Systems Command (page images at HathiTrust)
• Plasma oscillations. (Los Angeles, Physical Research Laboratory, Space Technology Laboratories, Inc., 1958), by John David Jackson (page images at HathiTrust)
• The damping of waves and other disturbances in mercury / ([Washington, D.C. : U.S. Dept. of Commerce, Bureau of Standards : U.S. Govt. Print. Off., 1917]), by Marcus Henry Stillman and United States. National Bureau of Standards (page images at HathiTrust)
• Flight evaluations of the effect of variable spiral damping in a JTB-26B airplane. (Buffalo, Cornell Aeronautical Laboratory, Inc., 1957), by Donald W. Rhoads (page images at HathiTrust)
• Aircraft motion sensitivity to cross and cross-coupling damping derivatives /, by R. W. Butler, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Roll-damping derivative calculations for spinning sharp and blunt cones in supersonic and hypersonic flow /, by Arloe W. Mayne, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• The effect of configurational additions using viscoelastic interfaces on the damping of a cantilever beam /, by James S. Whittier, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and sponsor University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Identification of dynamic structures with special attention to damping matrix representation /, by Jay H. Kim, sponsor Air Force Flight Dynamics Laboratory (U.S.), and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Proceedings of Damping '89 : 8-10 February 1989, West Palm Beach, Florida : final report for period Feb. 86 to Feb. 89 /, by Fla.) Damping '89 (1989 : West Palm Beach, sponsor Wright-Patterson Air Force Base (Ohio), sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)

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