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  • Large eddy simulations and turbulence modeling for film cooling [microform] / Sumanta Acharya.

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

  • 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

  • Experimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed [microform] / Douglas Thurman, Philip Poinsatte.

    • 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, 2000]
    • 2000

  • Prediction of film cooling on gas turbine airfoils [microform] / Vijay K. Garg and Raymond E. Grugler.

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

  • Experimental studies of shock-wave/wall-jet interaction in hypersonic flow [microform] / Michael S. Holden, Kathleen Rodriguez.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Center, distributor, 1994]
    • 1994

  • [FDNS code to predict wall heat fluxes or wall temperatures in rocket nozzles] [microform] : final report / prepared by Gerald R. Karr.

    • Text
    • Huntsville, AL : University of Alabama in Huntsville ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 8, Cooling flow/heat transfer analysis [microform] : users manual / E.J. Hall ... [et al.].

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

  • The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios [microform] / Kenneth J. Kacynski and Joe D. Hoffman.

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

  • Development of computer models for correlating data of film cooling of nose cone under hypersonic flow [microform] : semi-annual status report (April 1, 1986 to September 30, 1986) / principal investigator, L. Sharpe, Jr.

    • Text
    • Greensboro, NC : North Carolina A&T State University : [Washington, D.C. : National Aeronautics and Space Administration : Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Film cooling on a convex wall [microform] : heat transfer and hydrodynamic measurements for full and partial coverage / K. Furuhama ... [et al.].

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

  • 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

  • Leading edge film cooling effects on turbine blade heat transfer [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

  • Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream [microform] / George C. Olsen and Robert J. Nowak.

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

  • A numerical study of the effect of wake passing on turbine blade film cooling [microform] / James D. Heidmann.

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

  • Turbine vane external heat transfer [microform] : final report.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1985-
    • 1985-present

  • A performance comparison of two small rocket nozzles [microform] / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

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

  • The effect of wake passing on turbine blade film cooling [microform] / James David Heidmann.

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

  • NASA flow field analysis [microform] : final report / Charles L. Merkle.

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

  • Effect of coolant temperature and mass flow on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.

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

  • 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

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

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

  • 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

  • Coarse grid modeling of turbine film cooling flows using volumetric source terms [microform] / James D. Heidmann, Scott D. Hunter.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23040

  • Film cooling flow effects on post-combustor trace chemistry [microform] / Thomas Wey, Nan-Suey Liu.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS43886

  • Gas-jet and tangent-slot film cooling tests of a 12.5⁰ cone at Mach number of 6.7 [microform] / Robert J. Nowak.

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

    Available Online

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

  • Vortex generating flow passage design for increased film-cooling effectiveness and surface coverage [microform] / S. Stephen Papell.

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

  • Advanced liner-cooling techniques for gas turbine combustors [microform] / Carl T. Norgren and Steven [i.e. Stephen] M. Riddlebaugh.

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

  • Flow visualization study of the effect of injection hole geometry on an inclined jet in crossflow [microform] / Frederick F. Simon and Michael L. Ciancone.

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

  • Further shock tunnel studies of scramjet phenomena / R. G. Morgan ... [and others].

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS112727

  • Further shock tunnel studies of scramjet phenomena [microform] / R. G. Morgan ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112727

  • Perormance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydorgen-oxygen rocket [microform] / Lynn A. Arrington and Brian D. Reed.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]
    • 1992

  • Influence of coolant tube curvature on film cooling effectiveness as detected by infrared imagery / S. Stephen Papell, Robert W. Graham, and Richard P. Cageao.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1979.
    • 1979-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52212

  • Development of the Glenn Heat-Transfer (Glenn-HT) computer code to enable Time-Filtered Navier-Stokes (TFNS) simulations and application to film cooling on a flat plate through long cooling tubes / Ali Ameri [and five others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
    • 2014-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53708

  • Procedure for determining turbulence length scales using hotwire anemometry / Lamyaa A. El-Gabry, Douglas R. Thurman, Philip E. Poinsatte.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2014.
    • 2014-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo58001

  • Analysis of turbine blade relative cooling flow factor used in the subroutine coolit based on film cooling correlations / Steven J. Schneider.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2015.
    • 2015-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59984

  • Film cooling flow effects on post-combustor trace chemistry / Thomas Wey, Nan-Suey Liu.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2003.
    • 2003-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS43886

  • A performance comparison of two small rocket nozzles / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67112

  • A dual-plane PIV study of turbulent heat transfer flows / Mark P. Wernet and Adam C. Wroblewski, Randy J. Locke.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69048

  • The effect of wake passing on turbine blade film cooling / James David Heidmann.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70720

  • Experimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed / Douglas Thurman, Philip Poinsatte.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center : U.S. Army Research Laboratory, January 2000.
    • 2000-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo85942

  • Coarse grid modeling of turbine film cooling flows using volumetric source terms / James D. Heidmann, Scott D. Hunter.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2001.
    • 2001-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23040

  • Large Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer / Perry L. Johnson, Vikram Shyam.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32522

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