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  • Heat transfer on a film-cooled rotating blade [microform] / Vijay K. Garg.

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

  • Determination of a transient heat transfer property of acrylic using thermochromic liquid crystals [microform] / James D. Heidmann.

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

  • Development of a laser-induced heat flux technique for measurement of convective heat transfer coefficients in a supersonic flowfield [microform] / A. Robert Porro ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1991]
    • 1991

  • Transient hot-film sensor response in a shock tube [microform] / A.S. Roberts, Jr., K.R. Ortgies, and E. Gartenberg.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • 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

  • Bearing tester data compilation analysis, and reporting and bearing math modeling [microform] : monthly progress report for July, 1986.

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

  • Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.

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

  • Analysis of advanced solid rocket motor ignition phenomena [microform] : final report / by Winfred A. Foster, Jr., Rhonald M. Jenkins.

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

  • Heat transfer computations of internal flows with combined hydraulic and thermal developing length [microform] / C.R. Wang ... [et al.].

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

  • Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components [microform] : final technical report for NASA grant NAG 3-1796 / by principal investigator, Kenneth J. De Witt.

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

  • Calculation of multistage turbomachinery using steady characteristic boundary conditions [microform] / Rodrick V. Chima.

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

  • Heat transfer on a film-cooled blade [microform] : effect of hole physics : prepared under contract NAS3-27571 / Vijay K. Garg, David L. Rigby.

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

  • Heat transfer measurements on surfaces with natural ice castings and modeled roughness [microform] / K.S. Breuer ... [et al.].

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Calculation of multistage turbomachinery using steady characteristic boundary conditions [microform] / Rodrick V. Chima.

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

  • Heat transfer and flow on the first stage blade tip of a power generation gas turbine. Part 1, Experimental results [microform] / Ronald S. Bunker and Jeremy C. Bailey, Ali A. Ameri.

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

  • Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage [microform] / Louis M. Russell ... [et al.].

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

  • Comparison of thermal coefficients for two microwave detectors [microform] : diode/voltage-to-frequency converter and flash analog-to-digital converter / Anne I. Mackenzie.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27164

  • Heat transfer in a complex trailing edge passage for a high pressure turbine blade. Pt. 2, Simulation results [microform] / David L. Rigby, Ronald S. Bunker.

    • 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/LPS51556

  • The effect of cooling passage aspect ratio on curvature heat transfer enhancement [microform] / Michael L. Meyer.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS53769

  • Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel [microform] / Philip E. Poinsatte and G. James Van Fossen and Kenneth J. DeWitt ; prepared for the 28th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 8-11, 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/LPS69986

  • Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder [microform] / Kim A. Morehouse and Robert J. Simoneau.

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

  • Measurement of heat-transfer coefficients in shock wave-turbulent boundary layer interaction regions with a multi-layered thin film heat transfer gauge [microform] / Masanori Hayashi, Akira Sakurai and Shigeru Aso.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99340

  • Heat transfer distributions around nominal ice accretion shapes formed on a cylinder in the NASA Lewis icing research tunnel [microform] / G. J. Van Fossen, ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98924

  • Autoclave processing for composite material fabrication. 1 An analysis of resin flows and fiber compactions for thin laminate [microform] / T.H. Hou.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Channel flow modeling of impingement cooling of a rotating turbine blade [microform] / by JaHye Jenny Koo.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, [1984]
    • 1984

  • Sensitivity analysis of horizontal heat and vapor transfer coefficients for a cloud-topped marine boundary layer during cold-air outbreaks [microform] / by Yuwen Vaugn Chang.

    • Text
    • [Tallahassee, Fla.] : Florida State University College of Arts and Sciences ; [Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986

  • Evaluation of icing scaling on swept NACA 0012 airfoil models / Jen-Ching Tsao, Sam Lee.

    • Text
    • Brook Park, Ohio : Ohio Aerospace Institute ; Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2012.
    • 2012-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32879

  • In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 / Robert D. Quinn and Leslie Gong.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71370

  • Heat transfer computations of internal duct flows with combined hydraulic and thermal developing length / C.R. Wang [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, May 1997.
    • 1997-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72606

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