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  • A novel potential/viscous flow coupling technique for computing helicopter flow fields [microform] : final report / prepared by J. Michael Summa, Daniel J. Strash, Sungul Yoo.

    • Text
    • Redmond, WA : Analytical Methods, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1993

  • Control theory based airfoil design using the Euler equations [microform] / Antony Jameson and James Reuther.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade [microform] / T. Schobeiri, E. McFarland, and F. Yeh.

    • Text
    • [Washington, DC] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • Contraction design for small low-speed wind tunnels [microform] / J.H. Bell, R.D. Mehta ; prepared by Ames Research Center under Cooperative Agreement NCC-2-294.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, distributor, 1988]
    • 1988

  • Small-amplitude disturbances in turbomachine flows with swirl [microform] / David W. Wundrow.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Potential flow around two-dimensional airfoils using a singular integral method [microform] / by Yves Nguyen and Dennis Wilson.

    • Text
    • Austin, TX : Fluid Dynamics Group, Bureau of Engineering Research, University of Texas at Austin ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Combining comparison functions and finite element approximations in CFD [microform] / Kenneth J. Baumeister and Joseph F. Baumeister.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1955]
    • 1995

  • Potential flow downstream of the heliospheric terminal schock [microform] : a non-spherical schock / Steven Nerney and Steven T. Suess.

    • Text
    • Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Development of direct-inverse 3-D method for applied aerodynamic design and analysis [microform] : semiannual progress report, July 1, 1986 - December 31, 1986 / Leland A. Carlson.

    • Text
    • College Station, Tex. : Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Breakdown of the conservative potential equation [microform] / M.D. Salas and Clyde R. Gumbert.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1986.
    • 1986

  • Numerical solution of the full potential equation using a chimera grid approach [microform] / Terry L. Holst.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Control theory based airfoil design for potential flow and a finite volume discretization [microform] / J. Reuther and A. Jameson.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1995

  • On approximate factorization schemes for solving the full potential equation [microform] / Terry L. Holst.

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

  • Potential flow downstream of the heliospheric terminal shock [microform] : a non-spherical shock / Steven Nerney and S.T. Suess.

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

  • Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil [microform] / Dale Ashby.

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation [microform] / James Reuther ... [et al.].

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Study of the mutual interaction between a wing wake and an encountering airplane [microform] : NASA grant no. NAG1-1572, final report / by A.B. Walden, C.P. van Dam.

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

  • Application of a linearized unsteady aerodynamic analysis to standard cascade configurations [microform] / Joseph M. Verdon and William J. Usab, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics [microform] / Michael R. Wiese.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • Extension of transonic flow computational concepts in the analysis of cavitated bearings [microform] / D. Vijayaraghavan, T.G. Keith, Jr., and D.E. Brewe.

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60545

  • Discrete-vortex model for the symmetric-vortex flow on cones [microform] / Thomas G. Gainer.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65620

  • Unsteady potential flow past a propeller blade section [microform] / M.A. Takallu.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65495

  • A novel potential viscous flow coupling technique for computing helicopter flow fields [microform] / J. Michael Summa, Daniel J. Strash, Sungyul Yoo.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67056

  • A numerical analysis applied to high angle of attack three-dimensional inlets [microform] / Danny P. Hwang.

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

  • Trailing edge flow conditions as a factor in airfoil design [microform] / by A. I. Ormsbee and Mark D. Maughmer.

    • Text
    • Urbana, Ill. : Aeronautical and Astronautical Engineering Dept., University of Illinois ; [Washington, DC : National Aeronautics and Space Administration, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS86754

  • Numerical approach for the aerodynamic analysis of airfoils with laminar separation [microform] / prepared by David W. Halt and Dean R. Bristow.

    • Text
    • St. Louis, Mo. : McDonnel Douglas Corporation, McDonnel Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Delta wings with shock-free cross flow [microform] / S.S. Sritharan.

    • Text
    • Hampton, Va. : institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1984]
    • 1984

  • Entropy condtion satisfying approximations for the full potential equations of transonic flow [microform] / Stanley Osher, Woodrow Whitlow, Jr., and Mohamed Hafez.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / Daniel E. Paxson [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2015.
    • 2015-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62842

  • A vectorization of the Hess McDonnell Douglas potential flow program NUED for the Star-100 computer / Lillian R. Boney and Robert E. Smith, Jr.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1979.
    • 1979-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo172386

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