What altitude and temperature combination should be specified as a design point to ensure world-wide vertical flight capability for U.S. Army helicopters? This question was answered in 1970 by Robert Bellaire and Lieutenant William Bousman for the development of the Army's 2nd generation of helicopters (1970-1981). An update of the 1970 study is in progress. This update includes recent climatological and terrain data collected and processed by the use of the U.S.A.F. climatological model to represent areas between stations for a specific area. Regions of the world included in the 1970 study, as well as new relevant world regions are included in the new study.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Study of Army Design Hover Criteria


    Beteiligte:
    D. V. Horacek (Autor:in) / M. E. Calvert (Autor:in)

    Erscheinungsdatum :

    2017


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Study of the Army Hot Day Design Hover Criterion

    R. Bellaire / W. Bousman | NTIS | 1970


    Flight Evaluation Compliance Test Techniques for Army Hot Day Hover Criteria

    K. R. Ferrell / A. C. Frederickson / J. S. Kishi | NTIS | 1974


    Hover aircraft rotor and hover aircraft

    ATTILIO COLOMBO | Europäisches Patentamt | 2015

    Freier Zugriff

    Contra Rotating Hover Propeller Design

    Gur, Ohad / Silver, Jonathan / Dite, Radovan et al. | British Library Conference Proceedings | 2022


    Hover Testing of the NASA/Army/MIT Active Twist Rotor Prototype Blade

    Wilbur, M. L. / Yeager, W. / Wilkie, W. et al. | British Library Conference Proceedings | 2000