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  • The effects of vortex ingestion on the flow in a diffusing S-DUCT [microform] / B.J. Wendt and B.A. Reichert.

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

  • An aerodynamic analysis of a mixed flow turbine [microform] / Chan M. Kim and Kestutis C. Civinskas.

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

  • Numerical solution of the incompressible Navier-Stokes equations [microform] / Stuart E. Rogers.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Duct flow nonuniformities for space shuttle main engine (SSME) [microform] : final report / by Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center.

    • Text
    • Marshall Space Flight Center, AL : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Dual active surface heat flux gage probe [microform] / Curt H. Liebert and Paul Kolodziej.

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

  • Recent improvements to and validation of the one dimensional NASA wave rotor model [microform] / Daniel E. Paxson and Jack Wilson.

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

  • Study of compressible flow through a rectangular-to-semiannular transition duct / Jeffry Foster ... [et al.].

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

  • Thermodynamic evaluation of transonic compressor rotors using the finite volume approach [microform] : status report, August 1986 on NASA grant no. NAG 3-593 / by Stephen Nicholson, John Moore.

    • Text
    • Blacksburg, Va. : Mechanical Engineering Dept., Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Solution of the three-dimensional Helmholtz equation with nonlocal boundary conditions [microform] / Steve Hodge, William E. Zorumski, and Willie R. Watson.

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

  • Heat transfer computations of internal flows with combined hydraulic and thermal developing length [microform] / C.R. Wang ... [et al.].

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

  • Mixing of multiple jets with a confined subsonic crossflow [microform]. Part II, opposed rows of orifices in rectangular ducts / James D. Holdeman, David S. Liscinsky, Daniel B. Bain.

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

  • Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.].

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

  • The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct [microform] / Milo D. Dahl.

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

  • Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow [microform] / Kenneth J. Baumeister and Kevin L. Kreider.

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

  • Wave rotor demonstrator engine assessment [microform] / Philip H. Snyder.

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

  • Quick-mixing studies under reacting conditions [microform] : under grant NAG3-1110 / May Y. Leong and G.S. Samuelsen.

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

  • Experimental and theoretical study of flow fields around ducted-nacelle models [microform] / Robert J. Mack.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Perfectly matched layer for linearized Euler equations in open and ducted domains [microform] / C.K.W. Tam and L. Auriault, F. Cambuli.

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

  • An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct [microform] / B. A. Reichert and W. R. Hingst, and T. H. Okiishi.

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62060

  • Analysis of internal flow in a ventral nozzle for STOVL aircraft [microform] / C. Frederic Smith and Jack G. McArdle ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69189

  • Thermodynamic evaluation of transonic compressor rotors using the finite volume approach for the period 12/20/84 - 12/19/85 [microform] : annual report on NASA grant no. NAG 3-593 / by John Moore, Stephen Nicholson, Joan G. Moore.

    • Text
    • Blacksburg, Va. : Mechanical Engineering Dept., Virginia Polytechnic Institute and State University ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985]
    • 1985

  • A survey of oscillating flow in Stirling engine heat exchangers [electronic resource] / Terrence W. Simon and Jorge R. Seume.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113692

  • A survey of oscillating flow in Stirling engine heat exchangers [microform] / Terrence W. Simon and Jorge R. Seume.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113692

  • Mean veoIocity and turbulence measurements in a 90⁰ curved duct with thin inlet boundary layer [microform] : final report / R. A. Crawford ... [et al.].

    • Text
    • Tullahoma, Tenn. : University of Tennessee Space Institute, [1985]
    • 1985

  • Mean velocity and turbulence measurements in a 90° curved duct with thin inlet boundary layer : final report / R. A. Crawford ... [and others].

    • Text
    • Tullahoma, Tenn. : University of Tennessee Space Institute ; [Cleveland, Ohio] : NASA Lewis Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo22000

  • The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / Milo D. Dahl.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70672

  • Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow / Kenneth J. Baumeister and Kevin L. Kreider.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70683

  • Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length / C.R. Wang [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, May 1997.
    • 1997-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72606

  • Experimental and theoretical study of flow fields around ducted-nacelle models / Robert J. Mack.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83035

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