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  • Navier-Stokes dynamics and aeroelastic computations for vortical flows, buffet and aeroelastic applications [microform] / by Osama A. Kandil; principal investigator.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Analysis and control of asymmetric vortex flows and supersonic vortex breakdown [microform] : final report for the period December 1, 1991 to November 30, 1992 / Osama A. Kandil, principal investigator.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Analysis and control of asymmetric vortex flows and supersonic vortex breakdown [microform] / Osama A. Kandil, principal investigator.

    • Text
    • Norfolk, Va. : Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
    • 1991

  • Analysis and control of supersonic vortex breakdown flows [microform] / by Osama A. Kandil, principal investigator.

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

  • Unsteady hybrid vortex technique for transonic vortex flows and flutter applications [microform] / by Osama A. Kandil, principal investigator.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1986

  • Three dimensional solution of pneumatic active control of forebody vortex asymmetry [microform] / Osama A. Kandil and Hazem H. Sharaf El-Din, C.H. Liu.

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

  • Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications [microform] : final report for the period December 1, 1995 through Novemeber 30, 1996 / principal investigator, Osama A. Kandil ; submitted by the Old Dominion University Research Foundation.

    • Text
    • Norfolk, Va. : Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Effective control of computationally simulated wing rock in subsonic flow [microform] / Osama A. Kandil and Margaret A. Menzies.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet [microform] / Osama A. Kandil, Steven J. Massey and Essam F. Sheta.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes [microform] : 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA / Osama A. Kandil, Ihab Adam and Tin-Chee Wong.

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application [microform] : final report for the period of December 1, 1996-November 30, 1997 : under research grant NAG-1-648 / by Osama A. Kandil, principal investigator ; submitted by Old Dominion University Research Foundation.

    • Text
    • Norfolk, Va. : Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow [microform] / Osama A. Kandil, Essam F. Sheta, and Steven J. Massey.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1997]
    • 1997-1996

  • Computation and validation of fluid/structure twin tail buffet response [microform] / [Osama A. Kandil and Essam F. Sheta, C.H. Liu].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1997]
    • 1997-1996

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