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  • CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999 [microform] / edited by Woodrow Whitlow, Jr., Emily N. Todd ; proceedings of a workshop sponsored by the Confederation of European Aerospace Societies (CEAS), the American Institute of Aeronautics and Astronautics (AIAA), the National Aeronautics and Space Administration (NASA), Washington, D.C., and the Institute for Computer Applications in Science and Engineering (ICASE), Hampton, Virginia, and held in Williamsburg, Virginia, June 22-25, 1999.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver [microform] / T.S.R. Reddy and R. Srivastava, O. Mehmed.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : Available from National Technical Information Service, [1999]
    • 1999

  • Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation [microform] / T.S.R. Reddy ... [et al.].

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1992]
    • 1992

  • Some observations on the Houbolt-Rainey and peak-hold methods of flutter onset prediction [microform] / Robert V. Doggett, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1989

  • Shape sensitivity analysis of flutter response of a laminated wing [microform] / Fred D. Bergen and Rakesh K. Kapania.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, [1988]
    • 1988

  • Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model [microform] / José A. Rivera ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Additional development of the XTRAN3S computer program [microform] / C.J. Borland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Modern wing flutter analysis by computational fluid dynamics methods [microform] / Herbert J. Cunningham, John T. Batina, Robert M. Bennett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I [microform] / Michael W. Kehoe.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service], 1987.
    • 1987

  • Flutter analysis of composite box beams [microform] / Matthew Greenman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Improvements to the fastex flutter analysis computer code [microform] : final report, grant NAG 2-377 / Ronald F. Taylor.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Development of flight testing techniques [microform] : final report, 10/31/79 - 10/31/84 / principal investigator, Doral R. Sandlin.

    • Text
    • San Luis Obispo, CA : Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Flutter prediction for a wing with active aileron control [microform] : final report / principal investigators, Kevin Penning, Doral R. Sandlin.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University, Aeronautical Engineering Dept. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1983]
    • 1983

  • Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments [microform] / Robert V. Doggett, Jr., José A. Rivera, Jr., and Eric C. Stewart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Experimental classical flutter results of a composite advanced turboprop model [microform] / O. Mehmed and K.R.V. Kaza.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum I [microform] / J.D. Clayton and R.L. Haller.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum II [microform] / J.D. Clayton, R.L. Haller, and J.M. Hassler, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • FPCAS3D user's guide [microform] : full potential aeroelastic program / Milind A. Bakhle.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An interactive software for conceptual wing flutter analysis and parametric study [microform] / Vivek Mukhopadhyay.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • A presentation on robust flutter margin analysis and a flutterometer [microform] / Rick C. Lind.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • X-38 vehicle 131 flutter assessment [microform] / James P. Smith.

    • Text
    • [Houston, Tex.] : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Methods for in-flight robustness evaluation [microform] : summary of research / James D. Paduano, Eric Feron, Marty Brenner.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A worst-case approach for on-line flutter prediction [microform] / Rick C. Lind and Martin J. Brenner.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Robust flutter margin analysis that incorporates flight data [microform] / Rick Lind, Martin J. Brenner.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Application of TURBO-AE to flutter prediction [microform] : aeroelastic code development / Daniel Hoyniak, Todd A. Simons ; [prepared under contract NAS3-27725 task 6 EDR-19540].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • Optimization of training sets for neural-net processing of characteristic patterns from vibrating solids [microform] / Arthur J. Decker.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23330

  • Developing uncertainty models for robust flutter analysis using ground vibration test data [microform] / Starr Potter and Rick Lind.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22840

  • A probabilistic approach to model update [microform] / Lucas G. Horta, Mercedes C. Reaves, David F. Voracek.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27492

  • Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances [microform] / Lisa J. Bjarke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59777

  • The application of active controls technology to a generic hypersonic aircraft configuration [microform] / M.G. Gilbert ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69437

  • Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model [microform] / Walter A. Silva and Robert M. Bennett.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69438

  • Mass balancing of hollow fan blades [microform] / Robert E. Kielb.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Body-freedom flutter of a 1/2 scale forward-swept-wing-model, an experimental and analytical study [microform] / Richard Chipman, ... [et al.].

    • Text
    • Bethpage, N.Y. : Grumman Aerospace Corporation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88328

  • Analytical and experimental investigation of mistuning in propfan flutter [microform] / Krishna Rao V. Kaza ... [et al].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92416

  • Viscous effects on transonic airfoil stability and response [microform] / H. M. Berry, J. T. Batina, T. Y. Yang.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Exploratory flutter test in a cryogenic wind tunnel [microform] / Stanley R. Cole.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Ground vibration test results for drones for aerodynamic and structural testing (DAST)/aeroelastic research wing (ARW-1R) aircraft [microform] / Timothy H. Cox and Glenn B. Gilyard.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1986]
    • 1986

  • Flutter of swept fan blades [microform] / Robert E. Kielb and K. R. V. Kaza.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • An airfoil flutter model suspension system to accomdate large static transonic airloads [microform] / Wilmer H. Reed, III.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • An airfoil flutter model suspension system to accommodate large static transonic airloads / Wilmer H. Reed, III.

    • Text
    • Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo21276

  • Unsteady aerodynamic model tuning for precise flutter prediction / Chan-gi Pak.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24034

  • Basis function approximation of transonic aerodynamic influence coefficient matrix / Wesley W. Li and Chan-gi Pak.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24037

  • Modal filtering for control of flexible aircraft / Peter M. Suh, Dimitri N. Mavris.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54680

  • Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / Gregory P. Herrick.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2014.
    • 2014-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57922

  • Re-computation of numerical results contained in NACA report no. 496 / Boyd Perry, III.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2015.
    • 2015-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo60787

  • Flutter analysis of a transonic fan / R. Srivastava [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2002.
    • 2002-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS42474

  • Developing uncertainty models for robust flutter analysis using ground vibration test data / Starr Potter and Rick Lind.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2001.
    • 2001-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22840

  • Subsonic ultra green aircraft research phase II-volume I-3 / Marty K. Bradley, Christopher K. Droney, and Timothy J. Allen.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2014-2015.
    • 2014-2015
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62855

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