Research Catalog

  • Multistage simulations of the GE90 turbine [microform] / Mark G. Turner ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • MATE program. Volume II [microform] : erosion resistant compressor airfoil coating / Melvin Freling.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Experimental/analytical approach to understanding mistuning in a transonic wind tunnel compressor [microform] / Teri Kaiser ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Advanced turboprop wing installation effects measured by unsteady blade pressure and noise [microform] / Laurence J. Heidelberg and Richard P. Woodward ; prepared for the 11th Aeroacoustics Conference sponsored by the American Institute of Aeronautics and Astronautics, Sunnyvale, California, October 19-21, 1987.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • 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
  • [Thin film strain gage development program] [microform] : [final program].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1983]
    • 1983
  • Structural tailoring of engine blades (STAEBL), theoretical manual [microform] / K.W. Brown.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • Structural tailoring of engine blades (STAEBL), user's manual [microform] / K.W. Brown.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986
  • The measurement of boundary layers on a compressor blade in cascade at high positive incidence angle. II, Data report [microform] / Steve Deutsch and William C. Zierke.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986
  • The measurement of boundary layers on a compressor blade in cascade at high positive incidence angle. I, Experiment techniques and results [microform] / Steve Deutsch and William C. Zierke.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 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
  • 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
  • Development of a fiber optic compressor blade sensor [microform] : final report / principal investigator, Harbans Singh Dhadwal.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • 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
  • 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
  • The boundary layer on compressor cascade blades [microform] / submitted by Steven Deutsch and William C. Zierke.

    • Text
    • State College, PA : Applied Research Laboratory, The Pennsylvania State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1986]
    • 1986
  • Design procedures for compressor blades [microform] / H. Starken.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1983]
    • 1983
  • A model to assess the risk of ice accretion due to ice crystal ingestion in a turbofan engine and its effects on performance / Philip C. E. Jorgenson [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2013.
    • 2013-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53739

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