Research Catalog

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  • Steady secondary flows generated by periodic compression and expansion of an ideal gas in a pulse tube [microform] / Jeffrey M. Lee.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels [microform] / Milton Lamb.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Numerical analysis of intra-cavity and power-stream flow interaction in multiple gas-turbine disk-cavities [microform] / M.M. Athavale ... [et al.].

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

  • Turbomachinery design and tonal acoustics computations [microform] / Akil A. Rangwalla.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An investigation of bleed configurations and their effect on shock wave/boundary layer interactions [microform] : final report / Awatef Hamed, principal investigator.

    • Text
    • [Cincinnati, Ohio?] : University of Cincinnati ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Relative performance comparison between baseline labyrinth and dual-brush compressor discharge seals in a T-700 engine test [microform] / Robert C. Hendricks ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Adelphi, Md.] : U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A near-wall Reynolds-stress closure without wall normals [microform] : under grant NAG1-1772 / S.P. Yuan and R.M.C. So.

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

  • Aerodynamic synthesis of a centrifugal impeller using CFD and measurements [microform] / L.M. Larosiliere and G.J. Skoch, P.S. Prahst.

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

  • Flow simulation in secondary flow passages of a rocket engine turbopump [microform] : draft paper for 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio / Paul Schallhorn ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers [microform] / Bernhard H. Anderson, Dennis J. Keller.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26473

  • A three-dimensional CFD investigation of secondary flow in an accelerating, 90̊ elbow [microform] / Richard H. Cavicchi.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS29999

  • The effect of cooling passage aspect ratio on curvature heat transfer enhancement [microform] / Michael L. Meyer.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS53769

  • Effect of suction on controlling the secondary instability of boundary layers [microform] / Nabil M. El-Hady.

    • 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/LPS65496

  • Water flow measurements in a 180 degree turn-around duct [microform] / by V.A. Sandborn and J.C. Shin.

    • Text
    • Fort Collins, Colo. : Colorado State University, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69275

  • Secondary flow spanwise deviation model for the stators of NASA middle compressor stages [microform] / William B. Roberts and Donald M. Sandercock.

    • Text
    • Cleveland, Ohio : Lewis Research Center, [1984]
    • 1984

  • Double-branched vortex generator [microform] / Elizabeth R. Cantwell, Russell V. Westphal, R.D. Mehta.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Comparison of secondary flows predicted by a viscous code and inviscid code with experimental data for a turning duct [microform] / John R. Schwab and Louis A. Povinelli.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Aerodynamic synthesis of a centrifugal impeller using CFD and measurements / L.M. Larosiliere and G.J. Skoch, P.S. Prahst.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, July 1997.
    • 1997-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73188

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