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  1. 1
    Vibro-acoustics modal testing at NASA Langley Research Center

    Vibro-acoustics modal testing at NASA Langley Research Center by Pappa, Richard S.

    Published 1999
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  2. 2
    Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads

    Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads

    Published 1996
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  3. 3
    Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel

    Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel by Bird, R. Keith

    Published 1999
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  4. 4
    Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure /

    Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure / by Harris, Charles E., 1950-, Abeyounis, William Kelly

    Published 1996
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  5. 5
    Compression response of a sandwich fuselage keel panel with and without damage /

    Compression response of a sandwich fuselage keel panel with and without damage / by McGowan, David M., Ambur, Damodar R.

    Published 1997
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  6. 6
    Jet diffusion in proximity of a wall /

    Jet diffusion in proximity of a wall / by Küchemann, Dietrich, 1911-1976

    Published 1949
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  7. 7
    Rotor/body aerodynamic interactions

    Rotor/body aerodynamic interactions by Betzina, Mark D.

    Published 1983
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  8. 8
    Design of fuselage shapes for natural laminar flow /

    Design of fuselage shapes for natural laminar flow / by Dodbele, S. S.

    Published 1986
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  9. 9
    Damage arresting composites for shaped vehicles phase II final report /

    Damage arresting composites for shaped vehicles phase II final report /

    Published 2011
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  10. 10
    Methodology for predicting the onset of widespread fatigue damage in lap-splice joints /

    Methodology for predicting the onset of widespread fatigue damage in lap-splice joints / by Newman, J. C.

    Published 1998
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  11. 11
    Cabin fuselage structural design with engine installation and control system

    Cabin fuselage structural design with engine installation and control system

    Published 1994
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  12. 12
    Fuselage upwash effects on RSRA rotor systems

    Fuselage upwash effects on RSRA rotor systems by Cowan, J.

    Published 1985
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  13. 13
    The characterization of widespread fatigue damage in fuselage structure

    The characterization of widespread fatigue damage in fuselage structure by Piascik, Robert S.

    Published 1994
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  14. 14
    Estimation of dynamic rotor loads for the rotor systems research aircraft methodology development and validation /

    Estimation of dynamic rotor loads for the rotor systems research aircraft methodology development and validation / by Du Val, R. W.

    Published 1985
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  15. 15
    PRSEUS acoustic panel fabrication /

    PRSEUS acoustic panel fabrication / by Velicki, Alex

    Published 2011
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  16. 16
    Field-incidence transmission of treated orthotropic and laminated composite panels

    Field-incidence transmission of treated orthotropic and laminated composite panels by Koval, Leslie R.

    Published 1983
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  17. 17
    Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel /

    Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel / by Bird, R. Keith, Dicus, Dennis L.

    Published 1999
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  18. 18
    Study for prediction of rotor/wake/fuselage interference

    Study for prediction of rotor/wake/fuselage interference by Clark, D. R.

    Published 1985
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  19. 19
    Numerical study of three-dimensional separation and flow control at a wing-body junction progress report for the period ended April 30, 1989 /

    Numerical study of three-dimensional separation and flow control at a wing-body junction progress report for the period ended April 30, 1989 / by Lakshmanan, Balakrishnan, 1957-

    Published 1989
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  20. 20
    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept / by Wood, Richard M., Miller, David S. (Of Langley Research Center), Brentner, Kenneth S.

    Published 1983
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