IN the earliest stages of the development of the aeroplane the speed range obtainable was small, flight occurred only at fairly high lift coefficients, and induced drag was the predominant component of total resistance, hence successful flight depended on the achievement rather of minimum weight, minimum wing loading and maximum engine power than on the achievement of minimum possible parasite resistance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Air-Cooled Engine Cowling


    Untertitel :

    A Historical Survey with an Account of the Latest Work on the Townend Ring


    Beteiligte:
    North, J.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1934-04-01


    Format / Umfang :

    11 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Engine cowling with special reference to air-cooled engine

    North, J.D. | Engineering Index Backfile | 1934


    Engine cowling with special reference to air-cooled engine

    North, J.D. | Engineering Index Backfile | 1934


    Engine cowling with special reference to air-cooled engine

    North, J.D. | Engineering Index Backfile | 1934


    Engine cowling with special reference to air-cooled engine

    North, J.D. | Engineering Index Backfile | 1934


    ENGINE COWLING

    CIPRIAN ISPIR I | Europäisches Patentamt | 2017

    Freier Zugriff