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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    Titel :

    Practical airplane performance calculations


    Weitere Titelangaben:

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


    Beteiligte:
    Watter, M. (Autor:in)


    Erscheinungsdatum :

    1930


    Format / Umfang :

    18 pages


    Anmerkungen:

    48 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Part II. Practical Airplane Performance

    Lowry, John T. | AIAA | 1999


    Airplane vibration -- Practical approach

    Schultz, W.H. | Engineering Index Backfile | 1965


    Systems and methods for providing airplane performance calculations

    KIM GEUN IL / ALCANTARA ROY S / MALDONADO CHRISTIE M et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Airplane Performance Calculations by Means of Logarithmic Graphs

    Driggs, Ivan H. | SAE Technical Papers | 1938


    Systems and Methods for Providing Airplane Performance Calculations

    KIM GEUN II / ALCANTARA ROY S / MALDONADO CHRISTIE M et al. | Europäisches Patentamt | 2017

    Freier Zugriff