Method based on valuation of parasite resistance, wing or cell characteristics, and knowledge of engine propeller behavior, is intended for routine calculations; performance calculation includes maximum speed, stalling speed and service ceiling rate of climb at sea level and specified altitudes; climb in 10 min., time to climb to various altitudes, best speeds of climb, endurance at full throttle, range at full throttle, endurance at maximum range.


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    Title :

    Practical airplane performance calculations


    Additional title:

    Aeronautical Eng. (A.S.M.E. Trans.)


    Contributors:
    Watter, M. (author)


    Publication date :

    1930


    Size :

    18 pages


    Remarks:

    48 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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