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Vibration (Aeronautics)

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• Aeronautics
• Airplanes

• Buffeting (Aerodynamics)
• Flutter (Aerodynamics)

• Airplanes -- Vibration

• Measurement of low frequency vibrations in big helicopters and their transmission to the pilot / ([Washington, D.C. :] National Aeronautics and Space Administration, [1967]), by H. Seris and R. Auffret (page images at HathiTrust)
• Experimental dynamic stiffness and damping of externally pressurized gas-lubricated journal bearings / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by David P. Fleming, Robert E. Cunningham, William J. Thayer, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• A model and predictive scale of passenger ride discomfort / (Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1974), by Thomas K. Dempsey (page images at HathiTrust)
• On-line failure detection and damping measurement of aerospace structures by random decrement signatures / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Henry A. Cole, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• Ground and flight test methods for determining limit cycle and structural resonance characteristics of aircraft stability augmentation systems / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1972), by Weneth D. Painter, George J. Sitterle, and Flight Research Center (U.S.) (page images at HathiTrust)
• Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter / (Washington : National Aeronautics and Space Administration, [1960]), by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
• Effect of vertical active vibration isolation on tracking performance and ride qualities / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Frank P. DiMasi, Peter C. Calcaterra, Rush E. Allen, Langley Research Center, and Barry Wright Corporation (page images at HathiTrust)
• Interaction of the space shuttle control system with pogo / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by A. Stewart Hopkins, William F. Davis, Langley Research Center, and McDonnell Douglas Astronautics Company-Huntington Beach (page images at HathiTrust)
• The measurement and interpretation of ordinary power spectra for vibration problems / ([Washington] National Aeronautics and Space Administration, [1964]), by Allan G. Piersol, Measurement Analysis Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The development of vibration test specifications for spacecraft applications / ([Washington] : National Aeronautics and Space Administration, [1965]), by G. H. Klein, Allan G. Piersol, Measurement Analysis Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Compilation of shock and vibration flight data from eight Thor- related vehicles / ([Washington] : National Aeronautics and Space Administration, [1965]), by E. C. Meltzer, Douglas Aircraft Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hypersonic and transonic buzz measurements on the lower pitch flap of M2-F2 lifting entry configuration (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Robert W. Warner, Phillip R. Wilcox, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Instabilities in the flow of boiling liquid / ([Washington] : National Aeronautics and Space Administration, [1965]), by A. H. Stenning, T. Nejat Veziroglu, University of Miami, 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)
• An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades / (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 Aditi Chattopadhyay, Y. Danny Chiu, Langley Research Center, Lockheed Engineering & Sciences Company, and Inc Analytical Services & Materials (page images at HathiTrust)
• Experimental studies for determining human discomfort response to vertical sinusoidal vibration / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Thomas K. Dempsey, Jack D. Leatherwood, and Langley Research Center (page images at HathiTrust)
• Effect of high-velocity fluid flow on the bending vibrations and static divergence of a simply supported pipe / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Virginia 22151], 1965), by Harold L. Dodds, Harry L. Runyan, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Vibration handbooks for helicopters. (Washington, Distributed by the U.S. Dept. of Commerce. Office of Technical Services, 1954), by Robert A. Wagner (page images at HathiTrust)
• Vibrations measured in the passenger cabins of two jet transport aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by John J. Catherines, Harland F. Scholl, John S. Mixon, and Langley Research Center (page images at HathiTrust)
• Recent research on the determination of natural modes and frequencies of aircraft wing structures, (Washington, National Advisory Committee for Aeronautics, [1956]), by Langley Aeronautical Laboratory, John M. Hedgepeth, and United States. National Advisory Committee for Aeronautics. Advisory Group for Aeronautical Research and Development (page images at HathiTrust)
• RCS/linear discrete actuator study / (Edwards Air Force Base, Calif. : Air Force Astronautics Laboratory, Air Force Space Technology Center, Space Division, Air Force Systems Command, 1988), by Thomas Bailey, Paul Madden, Alexander Gruzen, Air Force Astronautics Laboratory (U.S.), and Charles Stark Draper Laboratory (page images at HathiTrust)
• Free vibration of a rotating beam-connected space station / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by James LaMar Milner and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Design of a precision tilt and vibration isolation system. ([Washington] National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Herbert Weinstock (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)
• Self-tuning regulators for multicyclic control of helicopter vibration / (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 Wayne Johnson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Application of a computerized vibroacoustic data bank for random vibration criteria development / (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 Robin C. Ferebee, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Vibration characteristics of OH-58A helicopter main rotor transmission / (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 David G. Lewicki, John J. Coy, United States. Army Aviation Research and Technology Activity. Propulsion Directorate, and Lewis Research Center (page images at HathiTrust)
• Derivation of a tapered p-version beam finite element / (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, 1989), by Howard E. Hinnant and Langley Research Center. Aerostructures Directorate (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)
• Testing of YUH-61A helicopter transmission in NASA Lewis 2240-kW (3000-hp) facility / (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 Andrew M. Mitchell, Fredrick T. Schuller, Fred B. Oswald, and Lewis Research Center (page images at HathiTrust)
• Aerodynamic roll damping of a T-tail transport configuration / (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)
• Human discomfort response to noise combined with vertical vibration / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Jack D. Leatherwood, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Richmond P. Boyden, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Noise transmission through plates into an enclosure / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Wayne B. McDonald, Michael K. Myers, Rimas Vaicaitis, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Rotor Systems Research Aircraft risk-reduction shake test / (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 J. Brent Wellman, United States. Army Aeroflightdynamics Directorate, and Ames Research Center (page images at HathiTrust)
• Ground vibration test of an F-16 airplane with modified decoupler pylons / (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 F. W. Cazier, M. W. Kehoe, and Langley Research Center (page images at HathiTrust)
• The vibration characteristics of a coupled helicopter rotor-fuselage by a finite element analysis / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Michael J. Rutkowski and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analysis of wing-body interaction flutter for a preliminary space shuttle design / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Richard R. Chipman, Peter Shyprykevich, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• Sensitivity analysis of torsional vibration characteristics of helicopter rotor blades / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1974]), by Theodore Bratanow, Akin Ecer, Langley Research Center, and University of Wisconsin--Milwaukee (page images at HathiTrust)
• Lunar orbiter flight vibration data and comparisons with environmental specifications [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Sherman A. Clevenson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Natural vibration and flutter of elastically supported corrugation-stiffened panels : experiment and theory [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1970), by Walter L. Heard, Herman L. Bohon, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic damping and oscillatory stability in pitch and yaw of Gemini configurations at Mach numbers from 0.50 to 4.63 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Bruce R. Wright, Robert A. Kilgore, and Langley Research Center (page images at HathiTrust)
• Tire stiffness and damping determined from static and free-vibration tests / (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 Robert K. Sleeper, Robert C. Dreher, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An assessment of the capability to calculate tilting prop-rotor aircraft performance, loads, and stability / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Wayne Johnson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Discomfort criteria for single-axis vibrations / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Thomas K. Dempsey, Sherman A. Clevenson, Jack D. Leatherwood, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A theoretical analysis of the free vibration of discretely stiffened cylindrical shells with arbitrary end conditions / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by D. M. Egle, K. E. Soder, University of Oklahoma, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of helicopter rotor blade torsional oscillations due to stall / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Peter Crimi, U.S. Army Air Mobility Research and Development Laboratory, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Transient excitation and mechanical admittance test techniques for prediction of payload vibration environments / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Daniel D. Kana, Luis M. Vargas, Southwest Research Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pogo suppression on space shuttle : early studies / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Stanley G. Rubin, J. G. Payne, W. G. Wagner, Langley Research Center, and Aerospace Corporation (page images at HathiTrust)
• Low-authority control synthesis for large space structures / (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 J. N. Aubrun, G. Margulies, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lockheed Missiles and Space Company, and Langley Research Center (page images at HathiTrust)
• Application of higher harmonic blade feathering on the OH-6A helicopter for vibration reduction / (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 F. K. Straub, E. V. Byrns, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center, and McDonnell Douglas Helicopter Company (page images at HathiTrust)
• Determination of subcritical frequency and damping from B-1 flight flutter test data / (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 Steven Kent Dobbs, C. H. Hodson, Hugh L. Dryden Flight Research Center, and Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• Instability of slender thin-walled booms due to thermally induced bending moments / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Vernon K. Merrick, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Psychophysical relationships characterizing human response to whole-body sinusoidal vertical vibration / (Washington : National Aeronautics and Space Administration ; Springfield, Va. for sale by the National Technical Information Service, 1976), by Jack D. Leatherwood, Thomas K. Dempsey, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Measured vibration response characteristics of four residential structures excited by mechanical and acoustical loadings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : Available through the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Huey P. Carden, William C. Mayes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analog analysis of the heave response and control of the plenum-type air-cushion vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Jack D. Leatherwood, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• The use of higher-order difference methods in beam vibration analysis / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Donald T. Greenwood, United States National Aeronautics and Space Administration, and University of Michigan. Dept. of Aeronautical and Astronautical Engineering (page images at HathiTrust)
• Vibration study of a pressurized torus shell / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Peter F. Jordan and Atis A. Liepins (page images at HathiTrust; US access only)
• Tensor analysis of aircraft structural vibration. ([New York], 1946), by Charles Edward Mack (page images at HathiTrust)
• Design of vibration isolation systems / (New York : Society of Automotive Engineers: Distribution [by] Pergamon Press, c1962), by SAE Committee G-5--Aerospace Shock and Vibration (page images at HathiTrust)
• Bibliography of vibration and flutter of aircraft wings and control surfaces, ([New York?], 1937), by United States. Work Projects Administration and Alexander Klemin (page images at HathiTrust)
• Uncoupled torsional vibrations of a thin, twisted, rotating beam /, by W. G. Brady, Walter P. Targoff, United States. Air Force. Air Research and Development Command. sponsor, Inc Cornell Aeronautical Laboratory, and Wright Air Development Center (page images at HathiTrust)
• Flutter investigation of two thin, low-aspect-ratio, swept, solid, metal wings in the transonic range by use of free-falling body / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by W. T. Lauten, Maurice A. Sylvester, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Hush House induced vibrations at the Arkansas Air National Guard Facility, Fort Smith, Arkansas / (Hanscom AFB, MA : Earth Sciences Division, Air Force Geophysics Laboratory, [1987]), by James C. Battis (page images at HathiTrust)
• Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by J. Cary Nettles, Robert C. Campbell, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Description and analysis of a rocket-vehicle experiment on flutter involving wing deformation and body motions / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by H. J. Cunningham, R. R. Lundstrom, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Moment of inertia and damping of fluid in tanks undergoing pitching oscillations / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Edward Widmayer, James R. Reese, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Atwood R. Heath, Robert L. O'Neal, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Flutter investigation of a true-speed dynamic model with various tip-tank configurations / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by John L. Sewall, William B. Igoe, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60©� delta-wing airplane model / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Lewis R. Fisher, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Damping in roll of models with 45©�, 60©�, and 70©� delta wings determined at high subsonic, transonic, and supersonic speeds with rocket -powered models / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by E. Claude Sanders, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Harry L. Runyan, Charles E. Watkins, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by John D. Bird, Sadie M. Hubbard, Lewis R. Fisher, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparative study of free and vast vibration analysis and computer programs / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation., 1961), by John Wallach, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• A slide rule type of device to measure logarithmic decay times as presented by oscillograph records / (Albuquerque, N.M. : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [1960]), by Rodman Leach, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
• Aries rocket flight vibration environment, TEM-2, multispectral measurements program /, by Russell G. Steeves and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Statistical techniques for describing localized vibratory environments of rocket vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], 1964), by Robert E. Barrett, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Large amplitude response of complex structures due to high intensity noise /, by C. Mei, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Application of the NASA kernel-function procedures to generally deforming wings /, by Bernard Mazelsky, Harry B. Armey, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Aerojet-General Corporation (page images at HathiTrust)
• Flight vibration survey of F-106A aircraft /, by H. Kent Reich and issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Random noise and vibration in space vehicles ([Alexandria, Va.] Shock and Vibration Information Center, U.S. Dept. of Defense: for sale by the Supt. of Docs., U.S. Govt. Print. Off., Washington, 1967), by Richard H. Lyon (page images at HathiTrust; US access only)
• Random vibration / (Cambridge, Mass. : M.I.T. Press, [1959, c1958]-1963), by Stephen H. Crandall (page images at HathiTrust)
• The design and development of the AFGL Vibro-Acoustic Measurement System /, by Howard E Michel and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Vibration of beams : a recurrence approach /, by Patrick M. Quinlan, United States. Air Force. Office of Scientific Research, and University College, Cork (page images at HathiTrust)
• Low frequency instabilities of free systems /, by Robert G. Schwendler, Jack H. Hill, Computer Engineering Associates. sponsor, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Wright-Patterson Air Force Base (Ohio), and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Viscoelastic support damping of built-in circular plates /, by T. J. Mentel, R. L. Schultz, sponsor University of Minnesota, sponsor Air Force Materials Laboratory (U.S.), sponsor Wright-Patterson Air Force Base (Ohio), and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• A guide for predicting the vibrations of fighter aircraft in the preliminary design stages /, by Eric E. Ungar, issuing agency Air Force Flight Dynamics Laboratory (U.S.), sponsor Grumman Aerospace Corporation, and Beranek Bolt (page images at HathiTrust)
• Bibliographical review of panel flutter and effects of aerodynamic noise /, by J. V. Rattayya, Lawrence E. Goodman, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Study of helicopter rotor-rotor interference effects on hub vibration /, by Jean Fernand Duvivier and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• A method for estimating damping derivatives of VTOL aircraft in transition and hovering flight /, by Paiewonsky Bernard H., sponsor United States. Air Force. Air Research and Development Command, and issuing body Wright Air Development Center (page images at HathiTrust)
• A study to correlate flight measured helicopter vibration data and pilot comments. /, by William J. Grant, Boeing Airplane Company. sponsor, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and United States. Air Force. Systems Command. Aeronautical Systems Division. issuing body (page images at HathiTrust)
• Vibrations in helicopters : training considerations /, by Robert J. Jr Randle, sponsor United States. Air Force. Air Research and Development Command, and issuing body Wright Air Development Center (page images at HathiTrust)
• Integrated passive and active control of structures /, by Vernon H. Neubert, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and sponsor Pennsylvania State University. Department of Engineering Sciences and Mechanics (page images at HathiTrust)
• A compilation of the mathematics leading to the doublet-lattice method /, by Max Blair and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)

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