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  • 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

  • Wave-rotor-enhanced gas turbine engine demonstrator [microform] / Gerard E. Welch ... [et al.].

    • 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

  • Experimental and numerical investigation of losses in low-pressure turbine blade rows [microform] / Daniel J. Dorney ... [et al.].

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

  • A combined experimental/computational study of flow in turbine blade cooling passage [microform] / D.G.N. Tse ... [et al.].

    • 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

  • Mars vertical axis wind machines [microform] : the design of a darreus and a gyromill for use on Mars.

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

  • 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

  • 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

  • Heat flux measurement in SSME turbine blade tester [microform]/ Curt H. Liebert.

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

  • Oxide-dispersion-strengthened turbine blades [microform] : materials for advanced turbine engines, project completion report, project 4 / by P.P. Millan, Jr. ... [et al.].

    • Text
    • [Phoenix, Ariz.] : Garrett Turbine Engine Co. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • User's manual for three dimensional boundary layer (BL3-D) code [microform] / by O.L. Anderson, B. Caplin.

    • Text
    • East Hartford, Conn. : United Technologies Research Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985

  • [Blade loss transient dynamics analysis. volume 2; task 2. tetra 2 user's manual [microform] : final report] / Gerald R. Black, Vincente C. Gallardo.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1986

  • [Blade loss transient dynamics analysis. volume 1; task 2, tetra 2 theoretical development [microform] : final report] / Vincente C. Gallardo, Gerald R. Black.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Design of test specimens and procedures for generating material properties of Douglas fir-epoxy laminated wood composite material, with the generation of baseline data at two environmental conditions [microform] : final report for period March 1982 through March 1985 / Paul E. Johnson.

    • Text
    • Dayton, Ohio : University of Dayton Research Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Modeling the effect of shroud contact and friction dampers on the mistuned response of turbopumps [microform] / J.H. Griffin and M-T. Yang.

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

  • Measurement of gust response on a turbine cascade [microform] : / A.P. Kurkov and B.L. Lucci.

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

  • Thermal barrier coating life-prediction model development [microform] : second annual report / by T.E. Strangman, J. Neumann, A. Liu.

    • Text
    • Phoenix, Ariz. : Garrett Turbine Engine Co. ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • A final report on NASA grant NSG 3079 entitled A linearized Euler analysis of unsteady flows in turbomachinery [microform] / by Kenneth C. Hall and Edward F. Crawley.

    • Text
    • Cambridge, MA : Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • An experimental study of near wall flow parameters in the blade end-wall corner region [microform] / Rakesh K. Bhargava and Rishi S. Raj.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1989.
    • 1989

  • 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

  • Turbine blade-tip clearance excitation forces [microform] : final report on Contract number NAS8-35018 / submitted by M. Martinez-Sanchez and Edward M. Greitzer to NASA, George C. Marshall Space Flight Center, Alabama.

    • Text
    • Cambridge, Mass. : Massachusetts Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • 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

  • Application of a personal computer for the uncoupled vibration analysis of wind turbine blade and counterweight assemblies [microform] / Phillip R. White and Ronald R. Little.

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

  • 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 and initial testing of a one-bladed 30-meter rotor on the NASA-DIE Mod-o wind turbine [microform] / R.D. Corrigan and C.B.F. Ensworth.

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

  • Design of an advanced wood composite rotor and development of wood composite blade technology [microform] / Thomas Stroeble, Curtis Dechow and Michael Zuteck.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • 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

  • Grid orthogonality effects on predicted turbine midspan heat transfer and performance [microform] / R.J. Boyle and A.A. Ameri.

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

  • Design and fabrication of forward-swept counterrotation blade configuration for wind tunnel testing [microform] : final report / prepared by G.H. Nichols.

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

  • Flow in serpentine coolant passages with trip strips [microform] : technical progress narrative report, reporting period September 1, 1995 to September 30, 1995 / D.G.-N. Lee.

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

  • Design protocols and analytical strategies that incorporate structural reliabilty models [microform] : final report / principal investigator, Stephen F. Duffy.

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

  • Reliability analysis of single crystal NiAl turbine blades [microform] / Joseph Palko ... [et al.].

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

  • Nonlinear analysis for high-temperature multilayered fiber composite structures [microform] / Dale A. Hopkins.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1984]
    • 1984

  • 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

  • Modeling the effect of shroud contact and friction dampers on the mistuned response of turbopumps [microform] : final report / J.H. Griffin and M-T. Yang.

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

  • Thermal and structural analysis of a hollow core Space Shuttle Main Engine (SSME) turbine blade [microform] / Ali Abdul-Aziz and Sreeramesh Kalluri, Michael A. McGaw.

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

  • Application of thin-film thermocouples to localized heat transfer measurements [microform] / J. Lepicovsky, R.J. Bruckner and F.A. Smith.

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

  • Oxide-dispersion-strengthened turbine blades [microform] / P.P. Millan, Jr., and J.C. Mays.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1986-
    • 1986-present

  • Endwall heat transfer measurements in a transonic turbine cascade [microform] / P.W. Giel ... [et al.].

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

  • Endwall heat transfer measurements in a transonic turbine cascade [microform] / P.W. Giel ... [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 mistuning on the forced response of turbomachinery rotors [microform] : a final report ... grant NAG3-1163 / principal investigator, Christophe Pierre.

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

  • Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine [microform] / Daniel J. Dorney.

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

  • Predicted turbine heat transfer for a range of test conditions [microform] / R.J. Boyle and B.L. Lucci.

    • Text
    • [Washington, D.C. : 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

  • 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

  • Structural evaluation of a space main engine (SSME) high pressure fuel turbopump turbine blade [microform] / Ali Abdul-Aziz.

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

  • Heat transfer experiments in the internal cooling passages of a cooled radial turbine rotor [microform] / B.V. Johnson and J.H. Wagner.

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

  • 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

  • Prediction of unshrouded rotor blade tip heat transfer [microform] : under cooperative agreement NCC3-370 / A.A. Ameri, E. Steinthorsson.

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

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