Damping (Mechanics) -- Equipment and suppliesSee also what's at your library, or elsewhere.
Broader terms:Narrower terms: |
Filed under: Damping (Mechanics) -- Equipment and supplies -- Materials -- Testing
Filed under: Damping (Mechanics) -- Automatic control -- Equipment and supplies -- Design and construction- Design and implementation of robust decentralized control laws for the ACES structure at Marshall Space Flight Center (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 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)
- High performance, accelerometer-based control of the mini-MAST structure at Langley Research Center (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Emmanuel G. Collins, Langley Research Center, and Harris Corporation. Government Aerospace Systems Division (page images at HathiTrust)
Items below (if any) are from related and broader terms.
Filed under: Damping (Mechanics)- Vibration isolation : use and characterization (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)
- Influence of damping in vibration isolation (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)
- Vibration control (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 (The Division :, 1979), 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 (The Commission :, 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)
- Evaluation of in-situ soil damping characteristics (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 ;, 1980), by Agbabian Associates, Shannon & Wilson, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
- Pipe damping-results of vibration tests in the 33 to 100 hertz frequency range (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)
- Experimental results from laboratory tests in the seismic range. (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)
- A digital instrumentation package for an improved torsion pendulum (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 (U.S. Dept. of the Interior, Bureau of Mines, 1987), by A. Visnapuu, P. C. Turner, and R. W. Nash (page images at HathiTrust)
- Properties of manganese-copper alloys prepared from metal powders (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 (U.S. Dept. of the Interior, Bureau of Mines, 1959), by J. W. Jensen (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 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1989, 1989), by Fla.) Damping '89 (1989 : West Palm Beach, Wright-Patterson Air Force Base (Ohio), Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
- Plasma oscillations. (Physical Research Laboratory, Space Technology Laboratories, Inc., 1958), by John David Jackson (page images at HathiTrust)
- Devices for damping mechanical vibrations, a bibliography. (Naval Research Laboratory, 1956), by Mildred Benton (page images at HathiTrust)
- Damping of rectangular plate vibrations (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)
- Flight evaluations of the effect of variable spiral damping in a JTB-26B airplane. (Cornell Aeronautical Laboratory, Inc., 1957), by Donald W. Rhoads (page images at HathiTrust)
- Damping of flexural vibrations by alternate visco-elastic and elastic layers (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 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 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 Air-Patterson Center, Air Research and Development Command, U. S. Air Force, 1959), by Theodore Joseph Mentel (page images at HathiTrust)
- The effect of configurational additions using viscoelastic interfaces on the damping of a cantilever beam (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1957), by James S. Whittier, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
- Response of bars (with internal and boundary damping) to transient and random excitation. (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1959), by Robert F. Lambert (page images at HathiTrust)
- The damping of waves and other disturbances in mercury (U.S. Dept. of Commerce, Bureau of Standards :, 1917), by Marcus Henry Stillman and United States. National Bureau of Standards (page images at HathiTrust)
- Seismic retrofit of existing concrete frame structures using viscoelastic damping devices (US Army Corps of Engineers, Construction Engineering Research Laboratory, 1995), by John R. Hayes and Construction Engineering Research Laboratory (page images at HathiTrust)
- Experimental evaluation of a tuned electromagnetic damper for vibration control of cryogenic turbopump rotors (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Eliseo DiRusso, Gerald V. Brown, and Lewis Research Center (page images at HathiTrust)
- Damping in tapered annular seals for an incompressible fluid (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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)
- An experimental investigation of the damping contribution of an elastomeric ablator on aluminum beams (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Robert E. Cunningham and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Dynamics and stability of mechanical systems with follower forces (National Aeronautics and Space Administration, 1971), by George Herrmann, United States. National Aeronautical and Space Administration, and Stanford University (page images at HathiTrust)
- Study and design of passive dampers for a manned rotating space station (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)
- Moment of inertia and damping of liquids in baffled cylindrical tanks (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 (National Aeronautics and Space Administration, 1966), by Luis R. Garza (page images at HathiTrust; US access only)
- Effect of support flexibility and damping on the dynamic response of a single mass flexible rotor in elastic bearings (National Aeronautics and Space Administration ;, 1972), by R. Gordon Kirk, Edgar J. Gunter, Lewis Research Center, and University of Virginia (page images at HathiTrust)
- Mechanical design handbook for elastomers (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)
- Predictions of F-111 TACT aircraft buffet response and correlations of fluctuating pressures measured on aluminum and steel models and the aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Charles F. Coe and Atlee M. Cunningham (page images at HathiTrust)
- An experimental investigation of the viscous damping of liquid sloshing in spherical tanks (National Aeronautics and Space Administration, 1963), by Irving E. Sumner, Andrew J. Stofan, and Lewis Research Center (page images at HathiTrust)
- NASA TR R-330 (National Aeronautics and Space Administration ;, 1970), by R. W. Hess, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- NASA TR R-249 (National Aeronautics and Space Administration ;, 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)
- Design of an oil squeeze film damper bearing for a multimass flexible-rotor bearing system (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 1974), by Richmond P. Boyden and Langley Research Center (page images at HathiTrust)
- Vibration of shaft face seals and stabilizing effect of viscous and friction damping (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 1968), by Rayjor W. H. Webeler, David C. Hammer, and Lewis Research Center (page images at HathiTrust)
- Effects of control-response characteristics on the capability of a helicopter for use as a gun platform (National Aeronautics and Space Administration :, 1960), by Robert J. Pegg, Andrew B. Connor, and Langley Research Center (page images at HathiTrust)
- Experimentally determined stiffness and damping of an inherently compensated air squeeze-film damper (National Aeronautics and Space Administration ;, 1975), by Robert E. Cunningham and Lewis Research Center (page images at HathiTrust)
- NASA TN D-5705 (National Aeronautics and Space Administration :, 1970), by Henry A. Cole, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Dynamic behavior of air lubricated pivoted-pad journal bearing - rotor system (National Aeronautics and Space Administration :, 1970), by Zolton N. Nemeth, William J. Anderson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5687 (National Aeronautics and Space Administration :, 1970), by Frank M. Bugg, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5508 (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)
- NASA TN D-5408 (National Aeronautics and Space Administration ;, 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)
- NASA TN D-3380 (National Aeronautics and Space Administration :, 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)
- Ring-baffle pressure distribution and slosh damping in large cylindrical tanks (National Aeronautics and Space Administration ;, 1972), by Harland F. Scholl, Phillip K. Davis, David G. Stephens, and Langley Research Center (page images at HathiTrust)
- NASA TN D-6526 (National Aeronautics and Space Administration ;, 1971), by Ted W. Nyland, Robert C. Anderson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Experimental investigation of the effect of model scale on structural-joint damping (National Aeronautics and Space Administration ;, 1967), by David G. Stephens, Maurice A. Scavullo, Brantley R. Hanks, and Langley Research Center (page images at HathiTrust)
- Experimental investigation of the slosh-damping effectiveness of positive-expulsion bags and diaphragms in spherical tanks (National Aeronautics and Space Administration, 1963), by Andrew J. Stofan and Irving E. Sumner (page images at HathiTrust)
- NASA TN D-3996 (National Aeronautics and Space Administration ;, 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)
- NASA TN D-1768 (National Aeronautics and Space Administration, 1963), by William R. Wehrend, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- NASA TN D-7066 (National Aeronautics and Space Administration ;, 1973), by Perry W. Hanson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NACA wartime reports (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)
- NACA wartime reports (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)
- 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 (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 (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 (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 (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)
- Shock-wave attenuation properties of a bubble screen (U). (Waterways Experiment Station, 1961), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
- Damping capacity of soil during dynamic loading : report 1 : review of mathematical material models (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 (U.S. Waterways Experiment Station ;, 1978), by Vincent P. Drnevich and Inc Soil Dynamics Instruments (page images at HathiTrust)
- Effect of material damping and stress distribution on the resonant fatigue strength of parts (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)
- Evaluation of S.D.R.C. damping analysis (The Office ;, 1980), by M. D. Noll, Structural Dynamics Research Corporation, and United States. Coast Guard. Office of Research and Development (page images at HathiTrust)
- On the law of damping of the luminescence of solid organic substances (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1954., 1954), by V. A. Yastrebov, U.S. Atomic Energy Commission, and National Science Foundation (U.S.) (page images at HathiTrust)
- Pneumatic isolation systems with linear passive damping (Livermore, California : Lawrence Livermore Laboratory, University of California, 1982., 1982), by D. B. DeBra, Richard E. Warner, and Lawrence Livermore Laboratory (page images at HathiTrust)
- Motions of a payload on a tethered, aerodynamic-shape balloon using various cable lengths (Hanscom AFB, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1975., 1975), by Don E. Jackson, Catherine B. Rice, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
- A Study of the effects of damping on normal modes of electrical and mechanical systems. (Washington, D. C. ; Air Research and Development Command, Office of Scientific Research, U.S. Air Force, 1955., 1955), by Stephen F. Crumb, California Institute of Technology, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
- Viscoelastic support junction damping of beams (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1961., 1961), by Theodore Joseph Mentel, C. C. Fu, R. L. Schultz, United States. Air Force. Air Research and Development Command, and Wright Air Development Division (page images at HathiTrust)
- Frictional damping and resonant vibration characteristics of an axial slip lap joint (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1954, 1954), by James H. Klumpp, Benjamin J. Lazan, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and University of Minnesota (page images at HathiTrust)
- A study of the rheological and damping properties of concrete (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)
- The damping of aluminum honeycomb sandwich beams (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by D. J. Mead, G. R. Froud, United States. Air Force. Systems Command. Aeronautical Systems Division, and University of Southampton (page images at HathiTrust)
- Cable and piston drag parameter investigation for hydraulic aircraft-arresting energy absorbers (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Howard L. Peterson, United States. Air Force. Systems Command. Aeronautical Systems Division, and United States. Air Force. Systems Command (page images at HathiTrust)
- A study to determine the effect of glass compositional variations on vibration damping properties (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Air Force Wright Aeronautical Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by George A. Graves, B. Kumar, Charles Cannon, Air Force Wright Aeronautical Laboratories, University of Dayton. Research Institute, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
- Analytical methods for determining specific damping energy considering stress distribution (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957., 1957), by E. R. Podnieks, B. J. Lazan, Wright Air Development Center, University of Minnesota, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
- Relationship between flutter parameters and generalized aerodynamic forces for wings of low aspect ratio (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Bernard Mazelsky, Harry B. Amey, United States. Air Force. Systems Command. Aeronautical Systems Division, and Aerojet-General Corporation (page images at HathiTrust)
- Experiments on slip damping at rounded contacts (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Directorate of Materials and Processes, Air Force Systems Command, United States Air Force, 1961., 1961), by L. E. Goodman, C. B. Brown, United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and University of Minnesota (page images at HathiTrust)
- Beam vibrations with quasi-orthogonal boundary conditions (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), by Y. C. Das, A. R. Robinson, Lawrence E. Goodman, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
- Identification of dynamic structures with special attention to damping matrix representation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1992., 1992), by Jay H. Kim, Air Force Flight Dynamics Laboratory (U.S.), and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
- Aircraft motion sensitivity to cross and cross-coupling damping derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by R. W. Butler, United States. Air Force. Systems Command, 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 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1979., 1979), by Arloe W. Mayne, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Multifrequency response of viscoelastic dampers (Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, 1967), by Ronald K. Newman, David C. Kraft, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
- Damping properties of viscoelastic materials under biaxial stress (Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, 1965), by Ahid D. Nashif, University of Dayton. Research Institute, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
- Energy dissipation in a vibration damper utilizing a viscoelastic suspension (Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965), by John P. Henderson and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
- Design of passive piezoelectric damping for space structures (National Aeronautics and Space Administration, Langley Research Center, 1994), by Nesbitt W. Hagood, Andreas H. von Flotow, Jack B. Aldrich, and Langley Research Center (page images at HathiTrust)
More items available under broader and related terms at left. |