Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • Theory of finite disturbances in a centrifuglal compression system with a vaneless radial diffuser [microform] / F.K. Moore.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • The effect of prewhirl on the internal aerodynamics nad performance of a mixed flow research centrifugal compressor [microform] / William B. Bryan and Sanford Fleeter.

    • Text
    • West Lafayette, Ind. : Thermal Sciences and Propulsion Center, School of Mechanical Engineering, Purdue University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Laser anemometer measurements of the three-dimensional rotor flow field in the NASA low-speed centrifugal compressor [microform] / Michael D. Hathaway ... [et al.].

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

  • Unsteady flow field in a multistage axial flow compressor [microform] / N. Suryavamshi, B. Lakshminarayana, J. Prato.

    • Text
    • University Park, PA : Center for Gas Turbine and Power, The Pennsylvania State University ; [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Coordinates for a high performance 4:1 pressure ratio centrifugal compressor [microform] / Ted F. McKain and Greg J. Holbrook.

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

  • Forced response testing of an axi-centrifugal turboshaft engine [microform] / A. Karl Owen ... [et al.].

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

  • Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor [microform] / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.

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

  • Wave augmented diffusers for centrifugal compressors [microform] / Daniel E. Paxson, Gary J. Skoch.

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

  • Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller [microform] / Lawrence F. Schumann, David A. Clark, and Jerry R. Wood.

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

  • Extended parametric representation of compressor fans and turbines [microform] / [G. L. Converse, R. G. Griffin].

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, Advanced Technology Programs Dept. ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984

  • Computational study of the CC3 impeller and vaneless diffuser experiment / Sameer Kulkarni, Timothy A. Beach, Gary J. Skoch.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55298

  • Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level / Edward P. Braunscheidel [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64050

  • Forced response testing of anaxi-centrifugal turboshaft engine / A. Karl Owen [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Adelphi, Maryland : U.S. Army Research Laboratory, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69828

  • Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70387

  • Progress of high efficiency centrifugal compressor simulations using TURBO / Sameer Kulkarni, Timothy A. Beach.

    • Text
    • Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79536

  • Rotary-wing relevant compressor aero research and technology development activities at Glenn Research Center / Gerard E. Welch ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo29187

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta