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  • Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft [microform] / submitted to NASA Lewis Research Center ; principal investigator Choon S. Tan, co-investigator Edward M. Greitzer.

    • Text
    • Cleveland, OH : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Inlet flow test calibration for a small axial compressor facility. Part I, Design and experimental results [microform] / D.P. Miller and P.S. Prahst.

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

  • Enhanced capabilities and modified users manual for axial-flow compressor conceptual design code CSPAN [microform] / Arthur J. Glassman and Thomas M. Lavelle.

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

  • NASA low-speed axial compressor for fundamental research [microform] / Charles A. Wasserbauer, Harold F. Weaver, Richard G. Senyitko.

    • 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

  • Compound cycle engine program [microform] / G.A. Bobula, W.T. Wintucky and J.G. Castor ; prepared for the Rotary Wing Propulsion System Specialist Meeting, sponsored by the American Helicopter Society, Williamsburg, Virginia, November 12-14, 1986.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • WINCLR [microform] : a computer code for heat transfer and clearance calculation in a compressor : a manual / T.K. Bose and S.N.B. Murthy.

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

  • Unsteady flows in a single-stage transonic axial-flow fan stator row [microform] / Michael D. Hathaway.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [St. Louis, MO] : U.S. Army Aviation Systems Command ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors [microform] : final report / by J.R. Gertz and A.H. Epstein.

    • Text
    • Cambridge, MA : Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • NASA low-speed axial compressor for fundamental research [microform] / Charles A. Wasserbauer, Harold F. Weaver, Richard G. Senyitko.

    • 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

  • Inlet flow test calibration for a small axial compressor rig. Part II, CFD compared with experimental results [microform] / D.P. Miller and P.S. Prahst.

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

  • The effect of adding roughness and thickness to a transonic axial compressor rotor [microform] / Kenneth L. Suder ... [et al.].

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

  • Design geometry and design/off-design performance computer codes for compressors and turbines [microform] / Arthur J. Glassman.

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

  • Static flow characteristics of a mass flow injecting valve [microform] / Duane Mattern and Dan Paxson.

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

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

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

  • Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance [microform] / Steven R. Wellborn and Theodore H. Okiishi.

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

  • PIV for turbomachinery applications [microform] / Mark P. Wernet.

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

  • Dimension determination of precursive stall events in a single stage high speed compressor [microform] / Michelle M. Bright, Helen K. Qammar and Tom T. Hartley.

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

  • 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

  • Aeropropulsion technology (APT) [microform] : task 23--stator seal cavity flow investigation / J.J. Heidegger, E.J. Hall, and R.A. Delaney.

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

  • Demonstration of PIV in a transonic compressor [microform] / Mark P. Wernet.

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

  • User's guide for MSAP2D [microform] : a program for unsteady aerodynamic and aeroelastic (flutter and forced response) analysis of multistage compressors and turbines : under grant NAG3-1137 / T.S.R. Reddy and R. Srivastava.

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

  • Small engine technology. Task 4, Advanced small turboshaft compressor (ASTC) performance and range investigation [microform] / Jeff L. Hansen and Robert A. Delaney.

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

  • Rotordynamics and design methods of an oil-free turbocharger [microform] / Samual A. Howard.

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

  • Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss / Kenneth L. Suder.

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

  • HPFTP flow diverter analysis [microform] : monthly progress report.

    • Text
    • Huntsville, Ala. : Huntsville Research & Engineering Center, [1985]
    • 1985

  • Investigation of axial positioning for flexural compressors [microform] : final technical report / Peter Riggle, principal investigator ; Daniel B. Olson, project engineer.

    • Text
    • Richland, WA : Tri-Cities University Center, University of Washington ; [Greenbelt, Md.] : Goddard Space Flight Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67021

  • 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

  • Design procedures for compressor blades [microform] / H. Starken.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1983]
    • 1983

  • Supersonic STOVL aircraft with turbine bypass/turbo-compressor engines [microform] / Leo C. Franciscus and Roger W. Luidens.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99531

  • Final report for the advanced turbocharger design study program [microform] / by D. G. Culy and R. W. Heldenbrand and N. R. Richardson.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984

  • Performance estimates for the space station power system Brayton Cycle compressor and turbine / Robert L. Cummings.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1989]
    • 1989

  • Performance estimates for the space station power system Brayton Cycle compressor and turbine / Robert L. Cummings.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1989.
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30314

  • An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor / Reid A. Berdanier and Nicole L. Key.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo65196

  • Dimension determination of precursive stall events in a single stage high speed compressor / Michelle M. Bright, Helen K. Qammar and Tom T. Hartley.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996.
    • 1996-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69462

  • Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project / Joseph P. Veres.

    • Text
    • Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2002.
    • 2002-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS46571

  • Methods for computationally efficient structured CFD simulations of complex turbomachinery flows / Gregory P. Herrick, Jen-Ping Chen.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo29068

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