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  • A comparison of experimental and theoretical results for labyrinth gas seals with honeycomb stators [microform] / by Lawrence Allen Hawkins.

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

  • Design of a low aspect ratio transonic compressor stage using CFD techniques [microform] / Nelson L. Sanger.

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

  • The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model [microform] : final report / R.P. Dring ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : National Technical Information Service, distributor], 1987.
    • 1987

  • Enhanced analysis and users manual for radial-inflow turbine conceptual design code RTD [microform] / Arthur J. Glassman.

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

  • Comparison of predicted low speed fan rotor/stator interaction modes to measured [microform] / Daniel L. Sutliff, James Bridges, Edmane Envia.

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

  • Effects of stator indexing on performance in a low speed multistage axial compressor [microform] / Wendy S. Barankiewicz and Michael D. Hathaway.

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

  • Energy efficient engine component development & integration program [microform] : semiannual report no. 7, April 1, 1981 - September 30, 1981 / General Electric project manager, R.W. Bucy.

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, Advanced Engineering and Technology Programs Dept. ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1981]
    • 1981

  • Actuator feasibility study for active control of ducted axial fan noise [microform] : under contract NAS3-26618 / John C. Simonich.

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

  • Reduced perceived noise low tip speed fans as result of abandoning cutoff stator vane numbers [microform] / James Dittmar.

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

  • Benefits of swept and leaned stators for fan noise reduction [microform] / Richard P. Woodward ... [et al.].

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

  • Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers [microform] / R.J. Boyle ... [et al.].

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

  • PSP measurement of stator vane surface pressures in a high speed fan [microform] / Jan Lepicovsky.

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

  • Design of a low speed fan stage for noise suppression [microform] / W.N. Dalton, D.B. Elliot, and K.L. Nickols.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Source methodology for turbofan noise prediction (SOURCED3D technical documentation) [microform] / Harold D. Meyer.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Performance improvement through indexing of turbine airfoils. Part 2, Numerical simulation [microform] / Lisa W. Griffin, Frank W. Huber and Om P. Sharma.

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

  • TFaNS Ṯone ̲F̲an Ṉoise Design/Prediction ̲System [microform] / David A. Topol.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999- ]
    • 1999-present

  • Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep [microform] / Donald B. Hanson ; prepared under contract NAS3-27727, AST task 13.

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

  • Stator and rotor flux based deadbeat direct torque control of induction machines [microform] / Barbara H. Kenny, Robert D. Lorenz.

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

  • Stator and rotor flux based deadbeat direct torque control of induction machines [microform] / Barbara H. Kenny, Robert D. Lorenz.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS45914

  • Simulating nonlinear stator noise for active control [microform] / R.W. Dyson ... [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, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55021

  • Three-dimensional Euler time accurate simulations of fan rotor-stator interactions [microform] / A.A Boretti.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60068

  • Radial and torsionally controlled magnetic bearing [microform].

    • Text
    • [Greenbelt, Md. : NASA Goddard Space Flight Center, 1985]
    • 1985

  • Analytical and experimental study of high phase order induction motors [microform] / Eugene A. Klingshirn.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS63456

  • Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading [microform] / Nelson L. Sanger and Raymond P. Shreeve.

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

  • Combined fringe and Fabry-Perot laser anemometer for three component velocity measurements in turbine stator cascade facility [microform] / Richard G. Seasholtz and Louis J. Goldman.

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

  • 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

  • A mathematical model for the doubly-fed wound rotor generator [microform] : part II / Frank J. Brady.

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

  • A simulation of rotor-stator interaction using the Euler equations and patched grids [microform] / Man Mohan Rai.

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

  • SSME seal test program : test results for sawtooth-pattern damper seal : interim progress report / prepared by Dara W. Childs.

    • Text
    • College Station, Tex. : Turbomachinery Laboratories, Mechanical Engineering Dept., Texas A & M University ; [Washington, D.C.] : [National Aeronautics and Space Administration], [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24439

  • SSME seal test program [microform] : test results for sawtooth-pattern damper seal : interim progress report / prepared by Dara W. Childs.

    • Text
    • College Station, Tex. : Turbomachinery Laboratories, Mechanical Engineering Dept., Texas A & M University ; [Washington, D.C. : National Aeronautics and Space Administration], [1986]
    • 1986

  • Comparison of predicted low speed fan rotor/stator interaction modes to measured / Daniel L. Sutliff, James Bridges, Edmane Envia.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, May 1996.
    • 1996-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72616

  • Simulink® controller for a reluctance motor with four-pole rotor and 36-tooth stator / Carlos R. Morrison and Andrew J. Provenza.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2017.
    • 2017-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82501

  • Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers / R.J. Boyle [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1998.
    • 1998-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83134

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