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  • Experimental measurements and analytical analysis related to gas turbine heat transfer [microform] : final report for NASA grant NAG3-581.

    • Text
    • Buffalo, N.Y. : Calspan-UB Research Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Theoretical, experimental, and computational evaluation of several vane-type slow-wave structures [microform] / Thomas M. Wallet and A. Haq Qureshi.

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

  • Validation of the F-18 high alpha research vehicle flight control and avionics systems modifications [microform] / Vince Chacon, Joseph W. Pahle, and Victoria A. Regenie.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Engine structures analysis software [microform] : component specific modeling (COSMO) / R.L. McKnight, R.J. Maffeo and S. Schwartz.

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

  • Turbulence and pressure loss characteristics of the inlet vanes for the 80-by 120-foot wind tunnel [microform] / Michael R. Dudley.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • The effect of swirl recovery vanes on the cruise noise of an advanced propeller [microform] / James H. Dittmar and David G. Hall.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Slow wave vane structure with elliptical cross-section slots, an analysis [microform] / Henry G. Kosmahl.

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

  • Experimental study of vane heat transfer and aerodynamics at elevated levels of turbulence [microform] / Forrest E. Ames.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Lateral jet injection into typical combustor flowfields [microform] / David G. Lilley.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986

  • Turbine blade and vane heat flux sensor development phase 2 [microform] / by W.H. Atkinson, M.A. Cyr, R.R. Strange.

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

  • Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle [microform] / W. Thomas Bundick ... [et al].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • 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

  • Experimental study of vane heat transfer and film cooling at elevated levels of turbulence [microform] / Forrest E. Ames.

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

  • 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

  • A three-dimensional coupled internal/external simulation of a film-cooled turbine vane [microform] / James D. Heidmann, David L. Rigby, Ali A. Ameri.

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

  • Comparison of predicted and measured turbine vane rough surface heat transfer [microform] / R.J. Boyle, C.M. Spuckler, and B.L. Lucci.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Infrared low temperature turbine vane rough surface heat transfer measurements [microform] / R.J. Boyle ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26729

  • Navier-Stokes analysis of turbine blade heat transfer [microform] / R.J. Boyle ; prepared for the 35th International Gas Turbine and Aeroengine Congress and Exposition sponsored by the American Society of Mechanical Engineers, Brussels, Belgium, June 11-14, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS66714

  • The structural dynamics analysis of the main injector LOX inlet tee and its redesign [microform] / [E. Romano].

    • Text
    • [Canoga Park, Calif. : Rockwell International, Rocketdyne Division? ; Washington, D.C. : National Aeronautics and Space Administration?, 1989?]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69840

  • Anisotropy of high temperature strength in precipitation-hardened nickel-base superalloy single crystals [microform] / Y. G. Nakagawa ... [et al.].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92737

  • Replaceable blade turbine and stationary specimen corrosion testing facility [microform] / Gilbert J. Santoro, Frederick D. Calfo, and Susan M. Benford.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985

  • Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [microform] / by H.T. Nagamatsu and R. E. Duffy.

    • Text
    • Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]
    • 1984

  • De-icing of the altitude wind tunnel turning vanes by electro-magnetic impulse [microform] / by Glen W. Zumwalt and Richard Ross.

    • Text
    • Wichita, Kan. : Aeronautical Engineering Department, Wichita State University ; Cleveland, Ohio : NASA Lewis Research Center, [1986]
    • 1986

  • Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle / W. Thomas Bundick [and three others]

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1996.
    • 1996-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67705

  • Comparison of predicted and measured turbine vane rough surface heat transfer / R.J. Boyle, C.M. Spuckler, and B.L. Lucci.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2000.
    • 2000-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79758

  • Infrared low temperature turbine vane rough surface heat transfer measurements / R.J. Boyle [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2000.
    • 2000-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79813

  • Liquid acquisition device design sensitivity study / M.K. Van Dyke, L.J. Hastings.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37676

  • Prediction of vortex-induced loads on wind tunnel turning vanes / James C. Ross.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, March 1985.
    • 1985-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173507

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