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  1. 1
    MAVRIC flutter model transonic limit cycle oscillation test

    MAVRIC flutter model transonic limit cycle oscillation test

    Published 2001
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  2. 2
    Response of the alliance 1 proof-of-concept airplane under gust loads

    Response of the alliance 1 proof-of-concept airplane under gust loads by Naser, A. S.

    Published 2001
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  3. 3
    Application of approximate unsteady aerodynamics for flutter analysis /

    Application of approximate unsteady aerodynamics for flutter analysis / by Pak, Chan-gi

    Published 2010
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  4. 4
    Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model /

    Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model / by Mahajan, Aparajit J.

    Published 1992
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  5. 5
    Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer /

    Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxid... by Pai, Shantaram S., Riha, David S.

    Published 2013
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  6. 6
    A presentation on robust flutter margin analysis and a flutterometer

    A presentation on robust flutter margin analysis and a flutterometer by Lind, Rick, 1968-

    Published 1997
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  7. 7
    Analysis of an unswept propfan blade with a semiempirical dynamic stall model /

    Analysis of an unswept propfan blade with a semiempirical dynamic stall model / by Reddy, T. S. R., Kaza, K. R. V.

    Published 1989
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  8. 8
    MAVRIC flutter model transonic limit cycle oscillation test /

    MAVRIC flutter model transonic limit cycle oscillation test / by Edwards, John W.

    Published 2001
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  9. 9
    Optical measurement of unducted fan flutter

    Optical measurement of unducted fan flutter by Kurkov, Anatole P.

    Published 1991
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  10. 10
    The use of the Regier number in the structural design with flutter constraints

    The use of the Regier number in the structural design with flutter constraints by Dunn, H. J., 1947-

    Published 1994
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  11. 11
    Aeroelasticity of wing and wing-body configurations on parallel computers

    Aeroelasticity of wing and wing-body configurations on parallel computers by Byun, Chansup

    Published 1995
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  12. 12
    Sensitivity analysis of flutter response of a wing incorporating finite-span corrections

    Sensitivity analysis of flutter response of a wing incorporating finite-span corrections by Issac, Jason Cherian

    Published 1994
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  13. 13
    Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model

    Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model by Turnberg, J. E.

    Published 1986
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  14. 14
    Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel : theory and experiment /

    Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel : theory and experiment / by Goldman, Benjamin D., Scott, Robert C., Dowell, E. H.

    Published 2014
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  15. 15
    A worst-case approach for on-line flutter prediction

    A worst-case approach for on-line flutter prediction by Lind, Rick, 1968-

    Published 1998
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  16. 16
    Final technical report for aeroelastic analysis of turbomachinery for space propulsion NASA grant number NAG3-1449, grant duration--January 13, 1993 to February 23, 1996 /

    Final technical report for aeroelastic analysis of turbomachinery for space propulsion NASA grant number NAG3-1449, grant duration--January 13, 1993 to February 23, 1996 / by Keith, Theo G.

    Published 1996
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  17. 17
    Improved flight test procedures for flutter clearance

    Improved flight test procedures for flutter clearance by Lind, Rick, 1968-

    Published 1997
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  18. 18
    Correlation filtering of modal dynamics using the Laplace wavelet

    Correlation filtering of modal dynamics using the Laplace wavelet by Freudinger, Lawrence C.

    Published 1997
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  19. 19
    Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996 /

    Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996 / by Keith, Theo G.

    Published 1997
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  20. 20
    ASTROP2 users manual : a program for aeroelastic stability analysis of propfans /

    ASTROP2 users manual : a program for aeroelastic stability analysis of propfans / by Reddy, T. S. R., Lucero, John M.

    Published 1996
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