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  1. 1
    The pressure available for ground cooling in front of the cowling of air-cooled airplane engines /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  2. 2
    Cooling tests of an airplane equipped with an NACA cowling and a wing-duct cooling system /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  3. 3
    Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
    by Holland, Scott Douglas, 1964-
    Published 1994

    Government Document Book
  4. 4
    The use of cowl camber and taper to reduce rotor/stator interaction noise
    by Martinez, R
    Published 1995

    Government Document Book
  5. 5
    Computational analysis in support of the SSTO flowpath test
    by Duncan, Beverly S
    Published 1994

    Government Document Book
  6. 6
    Ultra high bypass nacelle areodynamics inlet flow-through high angle of attack distortion test /
    by Larkin, Michael J
    Published 1992

    Government Document Book
  7. 7
    Drag and cooling with various forms of cowling for a Whirlwind engine in a cabin fuselage /
    by Weick, Fred E., Weick, Fred E.
    Published 1928

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  8. 8
    Concerning the flow about ring-shaped cowlings /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Book
  9. 9
    On wind tunnel tests and computations concerning the problem of shrouded propellers /
    by Krüger, W
    Published 1949

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    Wind-tunnel investigation of icing of an engine cooling-fan installation /
    by Lewis, James P
    Published 1947

    Government Document Book
  11. 11
    Comparative performance obtained with XF7C-1 airplane using several different engine cowlings /
    by Schey, Oscar W
    Published 1930

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  12. 12
    Drag tests of 4/9-scale model engine nacelles with various cowlings /
    by Windler, Ray
    Published 1932

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  13. 13
    Drag and cooling with various forms of cowling for a "Whirlwind" engine in a cabin fuselage /
    by Weick, Fred E
    Published 1928

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  14. 14
    Flight tests of N.A.C.A. nose-slot cowlings on the BFC-1 airplane /
    by Stickle, George W
    Published 1939

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  15. 15
    Development of a protected air scoop for the reduction of induction-system icing /
    by Von Glahn, Uwe
    Published 1946

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  16. 16
    The Pressure available for ground cooling in front of the cowling of airc-cooled airplane engines /
    by Stickle, George W
    Published 1938

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  17. 17
    Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction /

    Government Document Book
  18. 18
    Effect of the angular position of the section of a ring cowling on the high speed of an XF7C-1 airplane /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  19. 19
    Cooling tests of an airplane equipped with an NACA cowling and a wing-duct cooling system /
    by Turner, L. I
    Published 1941

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  20. 20
    Flight tests of N.A.C.A. nose-slot cowlings on the BFC-1 airplane /
    by Stickle, George W.
    Published 1939

    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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