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Flutter (Aerodynamics)

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• Transonic flutter investigation of models of proposed horizontal tails for the X-15 airplane / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Lou S. Young and Langley Research Center (page images at HathiTrust)
• Transonic flutter investigation of models of the X-15 airplane horizontal tail / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Lou S. Young, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
• Flutter of T-tails with dihedral : report on tests at David Taylor Model Basin. (Baltimore : Martin, [1957]), by R. L. Goldman (page images at HathiTrust; US access only)
• Comparative flutter calculations on low-aspect-ratio wings in incompressible and supersonic flows. ([Cambridge, Mass.] M.I.T. Department of Aeronautical Engineering, 1954), by Garabed Zartarian, Herbert M. Voss, and Pao Tan Hsu (page images at HathiTrust; US access only)
• Construction and testing of a doubly-flexible flutter model of a delta wing. ([Cambridge] M.I.T. Aeroelastic and Structures Research Laboratory, 1955), by Michael M. Chen (page images at HathiTrust; US access only)
• Flutter of low aspect-ratio wings. ([Cambridge, Mass.], 1957), by Massachusetts Institute of Technology (page images at HathiTrust; US access only)
• Effect of aerodynamic heating on the flutter of thin flat-plate arrow wings / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1963), by Joseph M. Groen, Richard Rosecrans, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Application of spring tabs to elevator controls / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by William H. Phillips, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Analytical study of shimmy of airplane wheels / (Washington, D.C. : NACA, 1952), by Christian Bourcier de Carbon and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces [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 Herbert J. Cunningham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and calculated results of a flutter investigation of some very low aspect-ratio flat-plate surfaces at Mach numbers from 0.62 to 3.00 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Dept. of Commerce, Washington, D.C. 20230], 1963), by Perry W. Hanson, Gilbert M. Levey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methods / (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 E. Nissim and Dryden Flight Research Facility (page images at HathiTrust)
• Modal interaction in linear dynamic systems near degenerate modes / ([Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]), by D. Afolabi and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aeroelastic modal characteristics of mistuned blade assemblies : mode localization and loss of Eigenstructure / ([Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]), by Christophe Pierre, Durbha V. Murthy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flutter of corrugation-stiffened panels at Mach 3 and comparison with theory / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Herman L. Bohon (page images at HathiTrust)
• Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by M. C. Sandford, Irving Abel, Charles L. Ruhlin, and Langley Research Center (page images at HathiTrust)
• An experimental study of the flutter of sails having a delta planform tested from a Mach number of 0.1 to a Mach number of 1.9 / (Washington [D.C.] : National Aeronautics and Space Administration, [1961]), by R. W. Hess, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flutter of panels on discrete flexible supports / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Manuel Stein and Langley Research Center (page images at HathiTrust)
• Method for experimental determination of flutter speed by parameter identification / (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 E. Nissim and Glenn B. Gilyard (page images at HathiTrust)
• Effect of control surface mass unbalance on the stability of a closed-loop active control system / (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 E. Nissim and Dryden Flight Research Facility (page images at HathiTrust)
• The effectiveness of vane-aileron excitation in the experimental determination of flutter speed by parameter identification / (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 E. Nissim and Dryden Flight Research Facility (page images at HathiTrust)
• Development of a nonlinear unsteady transonic flow theory / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Stephen S. Stahara, John R. Spreiter, Langley Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• Review of propeller-rotor whirl flutter / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Wilmer H. Reed, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Supersonic flutter of panels loaded with inplane shear / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by James Wayne Sawyer and Langely Research Center (page images at HathiTrust)
• Automated procedure for design of wing structures to satisfy strength and flutter requirements / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Raphael T. Haftka and Langley Research Center (page images at HathiTrust)
• Supersonic flutter of sandwich panels : effects of face sheet bending stiffness, rotary inertia, and orthotropic core shear stiffnesses / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Larry L. Erickson, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical calculations of two-dimensional, unsteady transonic flows with circulation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Richard M. Beam, Robert F. Warming, and Ames Research Center (page images at HathiTrust)
• Some effects of variations in density and aerodynamic parameters on the calculated flutter characteristics of finite-span swept and unswept wings at subsonic and supersonic speeds / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by E. Carson Yates and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept or unswept wings at subsonic, transonic, and supersonic speed / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by E. Carson Yates and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical calculations of velocity and pressure distribution around oscillating airfoils / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Theodore Bratanow, Michael Kobiske, Akin Ecer, Langley Research Center, and University of Wisconsin--Milwaukee (page images at HathiTrust)
• Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations / (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, 1991), by Donald F. Keller, Ellen Parker Bullock, and Langley Research Center (page images at HathiTrust)
• Study of the pressure distribution on oscillating panels in low supersonic flow with turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by E. F. E. Zeydel, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Development and applications of supersonic unsteady consistent aerodynamics for interfering parallel wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Kari Appa, G. C. C. Smith, Langley Research Center, and Bell Aerospace Company (page images at HathiTrust)
• Flutter of elastically supported orthotropic panels including the effects of flow angle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James Wayne Sawyer and Langley Research Center (page images at HathiTrust)
• Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jerrold M. Housner, Manuel Stein, and Langley Research Center (page images at HathiTrust)
• Experimental investigation of orthotropic panel flutter at arbitrary yaw angles, and comparison with theory / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Peter Shyprykevich, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• Theoretical study of camber flutter characteristics of monocoque and multiweb wings / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1962), by Robert G. Thomson, Edwin T. Kruszewski, 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)
• Transonic single-mode flutter and buffet of a low aspect ratio wing having a subsonic airfoil shape (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Larry L. Erickson, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Some effects of tip fins of wing flutter characteristics / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert C. Goetz, Robert V. Doggett, and Langley Research Center (page images at HathiTrust)
• Experimental parametric studies of transonic T-tail flutter / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Charles L. Ruhlin, M. C. Sandford, and Langley Research Center (page images at HathiTrust)
• Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by W. Jefferson Stroud, Manuel Stein, Cornelia B. Dexter, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils / (Washington, D.C. : National Aeronautical and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by F. Edward Ehlers, W. H. Weatherill, Boeing Commercial Airplane Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Some effects of fluid in pylon-mounted tanks on flutter / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by James R. Reese and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Supersonic flutter of airframes with flexible bodies, 24 April 1961 : final report 8 April 1960-7 April 1961 / (Kansas City, Mo. : Midwest Research Institute, [1961]), by John E. Yates and Edmond F. E. Zeijdel (page images at HathiTrust; US access only)
• Supersonic flutter of airframes with flexible bodies, 31 December 1962 : Final report 25 October 1961-24 November 1962. (Kansas City, Mo. : Midwest Research Institute, [1962]), by John E. Yates (page images at HathiTrust; US access only)
• Application of numerical integration techniques to the low-aspect-ratio flutter problem in subsonic and supersonic flows / ([Cambridge, Mass.] : Department of Aeronautical Engineering, Massachusetts Institute of Technology, 1954), by Herbert M. Voss, Garabed Zartarian, Pao Tan Hsu, and Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust; US access only)
• 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)
• Effects of leading-edge sweep on flutter characteristics of some delta-planform surfaces at a Mach number of 15.4 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1964), by Robert C. Goetz, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Synthesis of beam-network structures for low-aspect-ratio flutter models. ([Cambridge] M.I.T. Aeroelastic and Structures Research Laboratory, 1955), by Michael M. Chen and Sidney I. Gravitz (page images at HathiTrust; US access only)
• Experimenmtal flutter results for corrugation-stiffened and unstiffened panels / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Deene J. Weidman and Langley Research Center (page images at HathiTrust)
• Vibration and flutter tests of a pressurized thin-walled truncated conical shell / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Robert Miserentino, Sidney C. Dixon, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flutter, vibration, and buckling of truncated orthotropic conical shells with generalized elastic edge restraint / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Sidney C. Dixon, M. Latrelle Hudson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental panel flutter results for some flat and curved titanium skin panels at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by John G. Presnell, R. L. McKinney, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Comparison of analytical predictions of longitudinal short-period pilot-induced oscillations with results from a simulation study of the space shuttle orbiter / (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 Donald R. Riley, G. Kimball Miller, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• On curve veering and flutter of rotating blades / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993), by Dare Afolabi and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flutter analysis using transversality theory / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993), by D. Afolabi and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of preflutter and postflutter charactristics with motion-matched aerodynamic forces / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Herbert J. Cunningham, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An analytical technique for predicting the characteristics of a flexible wing equipped with an active flutter-suppression system and comparison with wind-tunnel data / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979), by Irving Abel (page images at HathiTrust)
• Application of model control to wing-flutter suppression / (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 Aaron J. Ostroff, Samuel Pines, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Robert F. O'Connell, N. A. Radovcich, H. J. Hassig, Lockheed-California Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Steady and unsteady aerodynamic forces from the SOUSSA surface-panel method for a fighter wing with tip missile and comparison with experiment and PANAIR / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Herbert J. Cunningham and Langley Research Center (page images at HathiTrust)
• Control surface spanwise placement in active flutter suppression systems / (Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988), by E. Nissim, John J. Burken, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Interstage adapter panel flutter on Atlas-Centaur AC-2, AC-3, and AC-4 vehicles / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1965), by Tilak R. Lall and Lewis Research Center (page images at HathiTrust)
• Experimental and analytical transonic flutter characteristics of a geared-elevator configuration / (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 Charles L. Ruhlin, Richard A. Gregory, Robert V. Doggett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Flutter analysis of an airplane with multiple structural nonlinearities in the control system / (Washington, D.C. : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Elmar J. Breitbach, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model / (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 Charles L. Ruhlin, K. S. Nagaraja, Kumar G. Bhatia, and Langley Research Center (page images at HathiTrust)
• Passive control of wing/store flutter / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Wilmer H. Reed, Jerome T. Foughner, F. W. Cazier, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A method to stabilize linear systems using Eigenvalue gradient information / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Carol D. Wieseman and Langley Research Center (page images at HathiTrust)
• Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 / (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 Jose A. Rivera (page images at HathiTrust)
• Analysis of an unswept propfan blade with a semiempirical dynamic stall model / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by T. S. R. Reddy and K. R. V. Kaza (page images at HathiTrust)
• ASTROP2 users manual : a program for aeroelastic stability analysis of propfans / (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 G. V. Narayanan, K. R. V. Kaza, and Lewis Research Center (page images at HathiTrust)
• Computer program for supersonic kernel-function flutter analysis of thin lifting surfaces / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Herbert J. Cunningham and Langley Research Center (page images at HathiTrust)
• Application of Zimmerman flutter-margin criterion to a wind-tunnel model / (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 Robert M. Bennett and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by John J. Adamczyk, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Development and application of an optimization procedure for flutter supression using the aerodynamic energy concept / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by E. Nissim, Irving Abel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods / (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 Lawrence C. Freudinger and Dryden Flight Research Facility (page images at HathiTrust)
• An experimental study of tip shape effects on the flutter of aft-swept, flat-plate wings / (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 Bryan E. Dansberry, Moses G. Farmer, Jose A. Rivera, and Langley Research Center (page images at HathiTrust)
• An experimental and analytical investigation of proprotor whirl flutter / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Raymond G. Kvaternik, Jerome S. Kohn, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Preliminary study of effects of winglets on wing flutter / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Robert V. Doggett, Moses G. Farmer, and United States National Aeronautics and Space Administration (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)
• Prediction of unsteady aerodynamic loadings caused by leading edge and trailing edge control surface motions in subsonic compressible flow : analysis and results / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by W. S. Rowe, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• A method for determining the characteristic functions associated with the aeroelastic instabilities of helicopter rotors in forward flight / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970), by Vincent James Piarulli, Richard P. White, United States National Aeronautics and Space Administration, Langley Research Center, and Rochester Applied Sciences Associates (page images at HathiTrust)
• Prediction of unsteady aerodynamic loadings caused by trailing edge control surface motions in subsonic compressible flow : analysis and results / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by W. S. Rowe, M. C. Redman, B. A. Winther, Langley Research Center, and Boeing Company (page images at HathiTrust)
• Analysis of stall flutter of a helicopter rotor blade / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Peter Crimi, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Harry L. Runyan, Nan H. Jones, and Langley Research Center (page images at HathiTrust)
• Experimental investigation of the influence of the turbulent boundary layer on the pressure distribution over a rigid two-dimensional wavy wall / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Lado Muhlstein, Richard G. Beranek, George C. Marshall Space Flight Center, and Ames Research Center (page images at HathiTrust)
• Flutter Research on skin panels / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Eldon E. Kordes, Lawrence D. Guy, W. J. Tuovila, and Langley Research Center (page images at HathiTrust)
• Flutter suppression using active controls based on the concept of aerodynamic energy [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1971), by E. Nissim, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flutter studies to determine nacelle aerodynamic effects on a fan-jet transport model for two mount systems and two wind tunnels [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 Moses G. Farmer, 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)
• An experimental study of the influence of the turbulent boundary layer on panel flutter / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Lado Muhlstein, Dennis W. Riddle, Peter A. Gaspers, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of the transonic flutter of simple thin truncated-cone panels / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Jean Gilman and Langley Research Center (page images at HathiTrust)
• Panel flutter studies of boost-vehicle full-scale flight insulation panels / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Michael L. Nacht, Richard L. Greene, and Lewis Research Center (page images at HathiTrust)
• Transonic and supersonic flutter trend investigation of a variable-sweep wing / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by John C. Stonesifer, Robert C. Goetz, and Langley Research Center (page images at HathiTrust)
• Thermoelastic damping and its effect on flutter of stressed panels situated in a supersonic airflow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by R. C. Shieh, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some effects of control profile and control trailing-edge angle on the oscillating hinge-moment and flutter characteristics of flap-type controls at transonic speeds / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by William C. Moseley, Thomas G. Gainer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of boundary-layer suction and spoilers on transonic flutter derivatives for a midspan control surface on an upswept wing / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Jone A. Wyss, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and calculated supersonic flutter characteristics of models of the x-15 horizontal and vertical tails / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by William T. Lauten, R. W. Hess, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Robert V. Doggett, Homer G. Morgan, A. Gerald Rainey, and Langley Research Center (page images at HathiTrust)
• Planform curvature effects on flutter characteristics of a wing with 56 ̊leading-edge sweep and panel aspect ratio of 1.14 / (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 Donald F. Keller, Theresa L. Pinkerton, M. C. Sandford, and Langley Research Center (page images at HathiTrust)
• Application of two design methods for active flutter suppression and wind-tunnel test results / (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 Jerry R. Newsom, H. J. Dunn, Irving Abel, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Generalization of the subsonic kernel function in the s-Plane, with applications to flutter analysis / (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 Herbert J. Cunningham, Robert N. Desmarais, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Formulation of blade-flutter spectral analyses in stationary reference frame / (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 Anatole P. Kurkov and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flutter of a low-aspect-ratio rectangular wing / (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 Stanley R. Cole and Langley Research Center (page images at HathiTrust)
• Flutter analysis and testing of pairs of aerodynamically interfering delta wings / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Richard R. Chipman, Frank J. Rauch, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• Development of an unsteady aerodynamic analysis for finite-deflection susonic cascades / (Washington, D.C. : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Joseph M. Verdon, Joseph R. Caspar, United Technologies Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Eigenspace techniques for active flutter suppression / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by William L. Garrard, Jerome A. Farm, and Bradley S. Liebst (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)
• Development and demonstration of a flutter-suppression system using active controls / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by M. C. Sandford, David L. Gray, Irving Abel, and Langley Research Center (page images at HathiTrust)
• Hypersonic flutter analysis using measured static aerodynamic derivatives, and comparison with experiment / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1969), by Robert C. Goetz, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flutter of buckled, simply supported, rectangular panels at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Robert W. Fralich, John A. McElman, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Further experimental results on the influence of the turbulent boundary layer on panel flutter / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Peter A. Gaspers, Daniel N. Petroff, Lado Muhlstein, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Development of a transfer function method for dynamic stability measurement / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Wayne Johnson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Application of the aerodynamic energy concept to flutter suppression and gust alleviation by use of active controls / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by E. Nissim, A. Caspi, I. Lottati, United States National Aeronautics and Space Administration, and Langley 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)
• Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane / (Washington, D.C. : National Aeronautics and Space Administration, 1969), by Maynard C. Sandford, Charles L. Ruhlin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Recent advances in aerodynamic energy concept for flutter suppression and gust alleviation using active controls. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by E. Nissim, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Flutter design of stiffened-skin panels for hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Herman L. Bohon, Walter L. Heard, Melvin S. Anderson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of the velocity fluctuations behind oscillating vanes / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Donald A. Buell, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Development of three-dimensional pressure-distribution functions for lifting surfaces with trailing-edge controls based on the integral equation for subsonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Alfredo Navarro Crespo, Herbert J. Cunningham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of limited amplitude and rate of flap motion on vane-controlled gust-alleviation system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by L. Keith Barker, Gene W. Sparrow, Daniel J. Crawford, Langley Research Center, 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)
• On the phenomenon of thermoelastic instability (thermal flutter) of booms with open cross section / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Richard M. Beam, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparative evaluation of methods for predicting flutter and divergence of unswept wings of finite span / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by E. Carson Yates, Samuel R. Bland, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flutter analysis of flat rectangular panels based on three-dimensional supersonic unsteady potential flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Herbert J. Cunningham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A theoretical analysis of the flutter of orthotropic panels exposed to a high supersonic stream of arbitrary direction / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Peter A. Gaspers, Bass Redd, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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)
• Flutter studies of simplified component models of a variable-sweep-wing airplane at Mach numbers up to 3.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by M. C. Sandford, Irving Abel, Charles L. Ruhlin, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Research on panel flutter / (Washington, D.C. : National Aeronautics and Space Administration, 1964), by D. R. Kobett (page images at HathiTrust; US access only)
• Flutter of multiple-streamwise bay rectangular panels at low supersonic mach number / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by D. R. Kobett (page images at HathiTrust; US access only)
• The flutter of flexible, towed tension shells / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Richard H. MacNeal (page images at HathiTrust; US access only)
• The flutter of towed rigid decelerators / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Richard H. MacNeal (page images at HathiTrust; US access only)
• Propeller blade stall flutter investigation. Contract no. AF 33(616)-2670. (Buffalo, Cornell Aeronautical Laboratory, Inc., 1958-), by William Gordon Brady (page images at HathiTrust)
• Supersonic flutter analyses including aerodynamic heating effects /, by R. L. Harder, United States. Air Force. Air Research and Development Command. sponsor, Wright Air Development Center issuing body, and Pasadena California Institute of Technology (page images at HathiTrust)
• Supersonic panel flutter /, by Yudell L. Luke, Andrew St. John, United States. Air Force. Air Research and Development Command. sponsor, Midwest Research Institute, and Wright Air Development Center (page images at HathiTrust)
• A study of wing flutter /, by A. F. Zahm, Ernest E. Wilson, United States. National Advisory Committee for Aeronautics, and United States. Navy. Bureau of Construction and Repair. Aerodynamical Laboratory (page images at HathiTrust)
• Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Dennis J. Martin, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (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)
• Discussion of three-dimensional oscillating air forces based on wind-tunnel measurements / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Sherman A. Clevenson, W. J. Tuovila, Sumner A. Leadbetter, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by George W. Jones, Hugh C. DuBose, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Some flutter experiments at a Mach number of 1.3 on cantilever wings with a tubular and closed bodes at the tips / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by John Locke McCarty, W. J. Tuovila, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Flutter characteristics of swept wings at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Laurence K. Loftin, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Exploratory investigation of the moments on oscillating control surfaces at transonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Dennis J. Martin, C. William Martz, Robert F. Thompson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Norman S. Land, Annie G. Fox, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Transonic flutter investigation of two 50©� semispan modified-delta wings with tip ailerons / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Robert J. Platt, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Determination of the performance parameters of a fluttering vane-type fuze-arming device using a controlled-geometry wind tunnel. (White Oak, Silver Spring, Md., Naval Ordnance Laboratory, [1970]), by Frank P. Baltakis, Paul J. Dawson, and Gary D. Senechal (page images at HathiTrust; US access only)
• 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)
• Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by WIlliam T. Lauten, Herbert C. Nelson, 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)
• Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by John L. Sewall, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• A preliminary wind-tunnel investigation of flutter characteristics of delta wings / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Robert W. Herr, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Preliminary study of some factors which affect the stall-flutter characteristics of thin wings / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by A. Gerald Rainey, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by William T. Lauten, Burke R. O'Kelly, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Flutter of a 60©� delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Joseph H. Judd, William T. Lauten, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Some experimental studies of panel flutter at Mach number 1.3 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Maurice A. Sylvester, John E. Baker, 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 compilation of experimental flutter information / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by H. J. Cunningham, Brown Harvey H., 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)
• Supersonic flutter of a 60©� delta wing encountered during the flight test of a rocket-propelled model / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by William T. Lauten, Joseph H. Judd, 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)
• 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 and theoretical studies of panel flutter at Mach number 1.2 to 3.0 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Maurice A. Sylvester, Herbert J. Cunningham, Herbert C. Nelson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by Albert P. Martina, 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)
• Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by George W. Jones, 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)
• Flutter at very high speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Harry L. Runyan, Homer G. Morgan, 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)
• 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)
• Effect of centrifugal force on flutter of uniform cantilever beam at subsonic speeds with application to compressor and turbine blades / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Alexander Mendelson and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Appraisal of method of flutter analysis based on chosen modes by comparison with experiment for cases of large mass coupling / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Donald S. Woolston, Harry L. Runyan, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some effects of density and Mach number on the flutter speed of two uniform wings / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by George E. Castile, Robert W. Herr, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transient aerodynamic behavior of an airfoil due to different arbitrary modes of nonstationary motions in a supersonic flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Chieh-Chien Chang and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An Iterative transformation procedure for numerical solution of flutter and similar characteristic-value problems / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Myron L. Gossard and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Harry L. Runyan and United States. National Advisory Committee for Aeronautics (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)
• Elimination of flutter in the radio flash code /, by Robert D Richtmyer, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Subsonic and transonic flutter and flow investigations of the T-tail of a large multijet cargo airplane / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Maynard C. Sanford, E. Carson Yates, Charles L. Ruhlin, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Subsonic and supersonic flutter analysis of a highly tapered swept-wing planform, including effects of density variation and finite wing thickness, and comparison with experiments / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by E. Carson Yates, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• Further studies on high-speed unsteady flow /, by Garabed Zartarian, Harry Sauerwein, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust)
• Active flutter suppression on an aeroelastically tailored HiMAT vehicle /, by John H. Wykes, issuing body United States. Air Force. Systems Command, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• Evaluations of methods to predict flutter of wings with external stores /, by Sidney Siegel, Lowell V. Andrew, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor North American Rockwell Corporation (page images at HathiTrust)
• 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)
• Subsonic flutter characteristics of a variable sweep wing and horizontal tail combination /, by Walter J. Mykytow, Michael H. Shirk, Lawrence J. Huttsell, Thomas E. Noll, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Supersonic speed flutter analysis of circular panels with edges elastically restrained against rotation /, by L. E. Goodman, Jasti Venkata Rattayya, sponsor University of Minnesota. Department of Aerospace Engineering and Mechanics, sponsor United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command. issuing body (page images at HathiTrust)
• Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 : supplement 1 /, by E. H. Dowell, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing body United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Boeing Company (page images at HathiTrust)
• Investigation of helicopter rotor blade flutter and flapwise bending response in hovering /, by Frank A. DuWaldt, R. A. Piziali, C. A. Gates, issuing body Wright Air Development Center, sponsor Cornell Aeronautical Laboratory, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Theoretical and experimental studies on airloads related to hypersonic aeroelastic problems of general slender pointed configurations /, by Garabed Zartarian, Pao Tan Hsu, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (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)
• Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 /, by E. H. Dowell, H. M. Voss, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Boeing Company (page images at HathiTrust)
• Basic principles of the indicial lifting-surface flutter-analysis procedure /, by Bernard Mazelsky, Harry B. Amey, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Aerojet-General Corporation (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)
• ASTROS enhancement final report /, by David L. Herendeen, D. J. Neill, Air Force Wright Aeronautical Laboratories. issuing body, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• Predicting the nonlinear response of aerospace structures using aeroelastic NS solutions on deforming meshes /, by Rathinam Panneer Selvam, Uday K. Roy, Qun Zheng, Zu-Qing Qu, Fayetteville. Civil Engineering University of Arkansas, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Experimental investigation of flutter in cascades with zero incidence and stagger /, by Robert J. Vaccaro, issuing body Wright Air Development Center, sponsor New York University. College of Engineering, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust; US access only)
• Reduced order modeling for aero-elastic simulations /, by M. J. Balas, sponsor University of Wyoming. Department of Electrical and Computer Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Admittance techniques in high speed flutter model testing., by Gifford W. Asher, Roy K. Watanabe, United States. Air Force. Systems Command. sponsor, United States. Air Force. Systems Command. Aeronautical Systems Division. issuing body, and Boeing Airplane Company. sponsor (page images at HathiTrust)
• Extend MANPADS M & S capabilities to include energetic materials, fragmentation effects, and wing flutter response /, by Ronald L. Hinrichsen, Brian D. Choules, Monty A. Moshier, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Fluid, structure and control interaction /, by Daniel J. Inman, Jens Cattarius, sponsor Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Department, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Flutter and vibration analysis by a modal method : analytical development and computational procedure /, by William P. Rodden, Heather A. Malcom, Edith F. Farkas, issuing body United States. Air Force. Systems Command. Space Systems Division, and sponsor Aerospace Corporation (page images at HathiTrust)
• The flutter of two-bay flat panels of infinite span at supersonic Mach numbers /, by M. H. Lock, Edith F. Farkas, issuing body United States. Air Force. Systems Command. Space Systems Division, and sponsor Aerospace Corporation. Laboratory Operations (page images at HathiTrust)
• ASTROS enhancements., by D. J. Neill, David L. Herendeen, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Influence of structural and aerodynamic modeling on flutter analysis and structural optimization /, by Alfred G. Struz, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and sponsor University of Oklahoma. School of Aerospace and Mechanical Engineering (page images at HathiTrust)
• ASTROS enhancements., by D. J. Neill, R. L. Hoesly, David L. Herendeen, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• ASTROS enhancements., by D. J. Neill, V. B. Venkayya, David L. Herendeen, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (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)
• A formulation of nonlinear limit cycle oscillation problems in aircraft flutter /, by Warren C. Chen, John Dugundji, issuing body United States. Air Force. Office of Scientific Research, and sponsor Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (page images at HathiTrust)
• Unsteady aerodynamics for advanced configurations., by M. T. Moore, L. V. Andrew, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• Experimental studies of the unstedy aerodynamics of panels at or near flutter with a finite boundary layer Mach number 1 to 10 /, by G. W. Asher, A. W. Brown, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Boeing Aerospace Company. sponsor (page images at HathiTrust)
• Commercial supersonic tansport panel flutter studies /, by C. H. Hodson, J. E. Stocker, North American Aviation. sponsor, United States. Federal Aviation Agency. sponsor, United States. Air Force. Systems Command. issuing body, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• ASTROS enhancement, by D. J. Neill, David L. Herendeen, Air Force Wright Aeronautical Laboratories. issuing body, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• Comparative experimental and theoretical studies of the flutter of flat panels in a low supersonic flow /, by M. H. Lock, Y. C. Fung, issuing body United States. Air Force. Office of Scientific Research, and sponsor California Institute of Technology (page images at HathiTrust)
• Unsteady aerodynamics for advanced configurations., by T. C. Li, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• ASTROS enhancement, by D. J. Neill, R. L. Hoesly, David L. Herendeen, Air Force Wright Aeronautical Laboratories. issuing body, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• Unsteady aerodynamics for advanced configurations., by E. R. Rodemich, L. V. Andrew, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• Unsteady aerodynamics for advanced configurations., by E. Albano, L. V. Andrew, United States. Air Force. Systems Command. issuing body, Air Force Flight Dynamics Laboratory (U.S.). sponsor, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• Real-time predictive flutter analysis and continuous paramter identification of accelerating aircraft /, by Charbel Farhat, University of Colorado Boulder. |b Department of Aerospace Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Validation tools of nonlinearities associated with aeroelastic phenomena /, by Muhammad R. Hajj, Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Department. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Experimental and calculated results of a flutter investigation of some very low aspect-ratio flat-plate surfaces at Mach numbers from 0.62 to 3.00 / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Perry W. Hanson, Gilbert M. Levey, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Tests of a wind tunnel flutter model., by Benjamin Smilg and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Effect of wing thickness and sweep on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by William C. Moseley, Thomas G. Gainer, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Research on panel flutter / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by D. R. Kobett, E. F. E. Zeydel, Mo.) Midwest Research Institute (Kansas City, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

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