Research Catalog

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  • Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation [microform] / T.S.R. Reddy ... [et al.].

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1992]
    • 1992

  • The WINCOF-I code [microform] : detailed description / S.N.B. Murthy and A. Mullican.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration : U.S. Dept. of Transportation, Federal Aviation Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines [microform] / Chung-Hua Wu.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Characteristics of an axisymmetric sudden expansion flow [microform] : progress report, 1 Jul. 1984 - 1 Jul. 1985 / W.H. Stevenson,and H.D. Thompson.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Laser doppler velocimeter system for subsonic jet mixer nozzle testing at the NASA Lewis Aeroacoustic Propulsion Lab [microform] / Gary G. Podboy ... [et al.].

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

  • Development of a linearized unsteady Euler analysis for turbomachinery blade rows [microform] / Joseph M. Verdon, Matthew D. Montgomery, and Kenneth A. Kourson.

    • 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

  • Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors [microform] : user's manual / James F. Schmidt.

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

  • Rotor vortex filaments [microform] : living on the slipstream's edge / Larry A. Young.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 199 ]
    • 1997

  • Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines [microform] / Om P. Sharma ... [et al.].

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

  • Numerical simulation of the generation of axisymmetric mode jet screech tones [microform] / H. Shen and C.K.W. Tam.

    • 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

  • Visualization of flows in packed beds of twisted tapes [microform] / R.C. Hendricks ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS42231

  • Laser anemometer measurements in a transonic axial-flow fan rotor [microform] / Anthony J. Stazisar ... [et al.].

    • 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], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68619

  • On the interaction of a sound pulse with the shear layer of an axisymmetric jet. III. Nonlinear effects [microform] / Alvin Bayliss, Lucio Maestrello, Eli Turkel.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, [1985]
    • 1985

  • Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile [microform] / Roy G. Stabe, Warren J. Whitney, and Thomas P. Moffitt.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99490

  • An experimental investigation of the impingement of a planar shock wave on an axisymmetric body at Mach 3 [microform] / A. Brosh and M. I. Kussoy.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983

  • Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams / Robert D. Ingebo.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981.
    • 1981-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71446

  • Visualization of flows in packed beds of twisted tapes / R.C. Hendricks [and four others].

    • Text
    • Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2002.
    • 2002-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS42231

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