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  1. 1
    A performance comparison of two small rocket nozzles /
    by Arrington, Lynn A
    Published 1996

    Government Document Book
  2. 2
    Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
    by Garg, V. K
    Published 1997

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  3. 3
    The effect of wake passing on turbine blade film cooling /
    by Heidmann, James D
    Published 1996

    Government Document Book
  4. 4
    Effect of coolant temperature and mass flow on film cooling of turbine blades
    by Garg, Vijay Kumar, 1938-
    Published 1997

    Government Document Book
  5. 5
    A numerical study of the effect of wake passing on turbine blade film cooling
    by Heidmann, James D
    Published 1995

    Government Document Book
  6. 6
    Experimental study of vane heat transfer and film cooling at elevated levels of turbulence
    by Ames, Forrest E
    Published 1996

    Government Document Book
  7. 7
    [FDNS code to predict wall heat fluxes or wall temperatures in rocket nozzles] final report /
    by Karr, Gerald R
    Published 1993

    Government Document Book
  8. 8
    Prediction of film cooling on gas turbine airfoils
    by Garg, Vijay Kumar, 1938-
    Published 1994

    Government Document Book
  9. 9
    Experimental studies of shock-wave/wall-jet interaction in hypersonic flow
    by Holden, Michael S
    Published 1994

    Government Document Book
  10. 10
    Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems users manual /
    Published 1994

    Government Document Book
  11. 11
    The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios /
    by Kacynski, Kenneth J
    Published 1994

    Government Document Book
  12. 12
    Development of computer models for correlating data of film cooling of nose cone under hypersonic flow semi-annual status report (April 1, 1986 to September 30, 1986) /
    by Sharpe, L
    Published 1987

    Government Document Book
  13. 13
    Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
    by Olsen, George C
    Published 1995

    Government Document Book
  14. 14
    Leading edge film cooling effects on turbine blade heat transfer
    by Garg, Vijay Kumar, 1938-
    Published 1995

    Government Document Book
  15. 15
    Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
    by Garg, Vijay Kumar, 1938-
    Published 1995

    Government Document Book
  16. 16
    Film cooling on a convex wall heat transfer and hydrodynamic measurements for full and partial coverage /
    Published 1985

    Government Document Book
  17. 17
    Film cooling flow effects on post-combustor trace chemistry /
    by Wey, Thomas
    Published 2003

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  18. 18
    Film cooling flow effects on post-combustor trace chemistry /
    by Wey, Thomas, Liu, Nan-Suey
    Published 2003

    Government Document Book
  19. 19
    Large eddy simulations and turbulence modeling for film cooling
    by Acharya, Sumanta
    Published 1999

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  20. 20
    Heat transfer on a film-cooled rotating blade
    by Garg, Vijay K
    Published 1999

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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