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  1. 1
    Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation

    Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation

    Washington, DC : National Aeronautics and Space Administration, 1992
    Format: Government Document Book


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  2. 2
    FPCAS3D user's guide : full potential aeroelastic program

    FPCAS3D user's guide : full potential aeroelastic program by Bakhle, Milind A.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Version 1.0.
    Format: Government Document Book


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  3. 3
    Shape sensitivity analysis of flutter response of a laminated wing

    Shape sensitivity analysis of flutter response of a laminated wing by Bergen, Fred D.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


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  4. 4
    X-38 vehicle 131 flutter assessment

    X-38 vehicle 131 flutter assessment by Smith, James P.

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


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  5. 5
    A worst-case approach for on-line flutter prediction

    A worst-case approach for on-line flutter prediction by Lind, Rick C.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  6. 6
    Improvements to the fastex flutter analysis computer code : final report, grant NAG 2-377

    Improvements to the fastex flutter analysis computer code : final report, grant NAG 2-377 by Taylor, Ronald F.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


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  7. 7
    A presentation on robust flutter margin analysis and a flutterometer

    A presentation on robust flutter margin analysis and a flutterometer by Lind, Rick C.

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


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  8. 8
    Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model

    Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model by Silva, Walter A.

    Hampton, Va. :; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990
    Format: Government Document Book


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  9. 9
    Flutter prediction for a wing with active aileron control : final report

    Flutter prediction for a wing with active aileron control : final report by Penning, Kevin

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


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  10. 10
    The application of active controls technology to a generic hypersonic aircraft configuration

    The application of active controls technology to a generic hypersonic aircraft configuration

    Hampton, Va. :; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990
    Format: Government Document Book


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  11. 11
    Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum II

    Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum II by Clayton, J. D.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  12. 12
    Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model

    Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1991
    Format: Government Document Book


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  13. 13
    Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum I

    Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum I by Clayton, J. D.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  14. 14
    Application of TURBO-AE to flutter prediction : aeroelastic code development

    Application of TURBO-AE to flutter prediction : aeroelastic code development by Hoyniak, Daniel

    [Cleveland, Ohio] : Hanover, Md. : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001
    Format: Government Document Book


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  15. 15
    An interactive software for conceptual wing flutter analysis and parametric study

    An interactive software for conceptual wing flutter analysis and parametric study by Mukhopadhyay, Vivek

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  16. 16
    A probabilistic approach to model update

    A probabilistic approach to model update by Horta, Lucas G.

    Hampton, Va. : Hanover Md. :; Hampton, Va. : Hanover MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2001
    Format: Government Document Book


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  17. 17
    Flutter analysis of composite box beams

    Flutter analysis of composite box beams by Greenman, Matthew

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  18. 18
    Modern wing flutter analysis by computational fluid dynamics methods

    Modern wing flutter analysis by computational fluid dynamics methods by Cunningham, Herbert J.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


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  19. 19
    Additional development of the XTRAN3S computer program

    Additional development of the XTRAN3S computer program by Borland, Christopher J.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1989
    Format: Government Document Book


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  20. 20
    Robust flutter margin analysis that incorporates flight data

    Robust flutter margin analysis that incorporates flight data by Lind, Rick, 1968-

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


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