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title: national advisory committee for aeronautics -- report

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    Charts for determining characteristics of sharp-nose airfoils in two-dimensional flow at supersonic speeds

    Ivey, H.R. / Stickle, G.W. / Schuettler, A. | Engineering Index Backfile | 1947
    Publisher: National Advisory Committee for Aeronautics

    Effect of altitude on cooling

    Brevoort, M.J. / Joyner, U.T. / Wood, G.P. | Engineering Index Backfile | 1943
    Publisher: National Advisory Committee for Aeronautics

    Experimental investigation of entrance-region heat-transfer coefficients

    Joyner, U.T. | Engineering Index Backfile | 1943
    Publisher: National Advisory Committee for Aeronautics

    Pressure available for cooling with cowling flaps

    Stickle, G.W. / Naiman, I. / Crigler, J.L. | Engineering Index Backfile | 1941
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Problem of cooling air-cooled cylinder on aircraft engine

    Brevoort, M.J. / Joyner, U.T. | Engineering Index Backfile | 1941
    analyzed on basis of effectiveness in cooling with respect to power for cooling; altitude problem is analyzed for both supercharged and ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Propeller analysis from experimental data

    Stickle, G.W. / Crigler, J.L. | Engineering Index Backfile | 1941
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Effect of body nose shape on propulsive efficiency of propeller

    Stickle, G.W. / Crigler, J.L. / Naiman, I. | Engineering Index Backfile | 1941
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Effect of exit-slot position and opening on available cooling pressure for N.A.C.A. Nose-slot cowlings

    Stickle, G.W. / Naiman, I. / Crigler, J.L. | Engineering Index Backfile | 1940
    available for cooling; engine conductances from 0 to 0.12 and exit slot conductances from 0 to 0.30 covered. ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Design of N.A.C.A. Cowlings for radial air-cooled engines

    Stickle, G.W. | Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Cooling on front of air-cooled engine cylinder in conventional engine cowling

    Brevoort, M.J. / Joyner, U.T. | Engineering Index Backfile | 1939
    Measurements made of cooling on fronts of model cylinders in conventional cowling for cooling in both ground and cruising conditions ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

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