31–40 of 3,338 hits
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    Effect of six aromatic amines on preignition-limited performance of 28-R aviation fuel in CFR engine

    Male, D.W. | Engineering Index Backfile | 1945
    Effect of Six Aromatic Amines on Preignition-Limited Performance of 28-R Aviation Fuel in CFR Engine (Originally issued as Memorandum ...

    The comparative performance of an aviation engine at normal and high inlet air temperatures

    Gardiner, A.W. / Schey, O.W. | Engineering Index Backfile | 1927
    Relation between power and temperature for carburetor air temperatures encountered when super-charging to sea-level pressure at altitudes ...
    Publisher: National Advisory Committee for Aeronautics

    Suitability of ethers as aviation fuel components -- Knock-limited performance of several ethers blended with an-F-28 fuel

    Alquist, H.E. / Tower, L.K. | Engineering Index Backfile | 1945
    Suitability of ethers as aviation fuel components -- Knock-limited performance of several ethers blended with an-F-28 fuel. (Confidential ...
    Publisher: National Advisory Committee for Aeronautics

    PREPARATION OF SAE TECHNICAL REPORTS—SURFACE VEHICLES AND MACHINES: STANDARDS, RECOMMENDED PRACTICES, INFORMATION REPORTS

    SAE Technical Papers | 1979
    for interpretation or for discussion by the full Publications Advisory Committee. The rationale which accompanies a technical report when ...
    Keywords: Aviation fuels

    Correlation of effects of compression ratio and inlet-air temperature on knock limits of aviation fuels in CFR engine -- I

    Evvard, J.C. / Branstetter, J.R. | Engineering Index Backfile | 1945
    Correlation of effects of compression ratio and inlet-air temperature on knock limits of aviation fuels in CFR engine -- I. (Advance ...
    Publisher: National Advisory Committee for Aeronautics

    Correlation of effects of compression ratio and inlet-air temperature on knock limits of aviation fuels in CFR engine -- II

    Alquist, H.E. / O'Dell, L. / Evvard, J.C. | Engineering Index Backfile | 1946
    Correlation of effects of compression ratio and inlet-air temperature on knock limits of aviation fuels in CFR engine -- II. (Advance ...
    Publisher: National Advisory Committee for Aeronautics

    Airfoil section characteristics as affected by variations of Reynolds Number

    Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937
    Publisher: National Advisory Committee for Aeronautics

      Airfoil section characteristics as affected by variations of Reynolds Number

      Jacobs, E.N. / Sherman, A. | Engineering Index Backfile
      characteristics with changes in Reynolds Number are inferred and methods of allowing for these variations in practice determined. ...
      Publisher: National Advisory Committee for Aeronautics

      Airfoil section characteristics as affected by variations of Reynolds Number

      Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937
      Publisher: National Advisory Committee for Aeronautics

    Report on ice formation on aircraft -- By French committee for study of ice formation

    Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Experimental studies of knock-limited blending characteristics of aviation fuels -- II: investigation of leaded paraffinic fuels in air-cooled cylinder

    Wear, J.D. / Sanders, N.D. | Engineering Index Backfile | 1947
    20 supp sheets. Relation between knock limit and blend composition of selected aviation fuel components individually blended with virgin ...
    Publisher: National Advisory Committee for Aeronautics

    Correlation of effects of fuel-air ratio, compression ratio, and inlet-air temperature on knock limits of aviation fuels

    Tower, L.K. / Alquist, H.E. | Engineering Index Backfile | 1950
    Correlation of Effects of Fuel-Air Ratio, Compression Ratio, and Inlet-Air Temperature on Knock Limits of Aviation Fuels. ...
    Publisher: National Advisory Committee for Aeronautics