A reduction in helicopter parasite drag is possible but not profitable except in those cases where high speed and long range are primary requirements . For some of the factors causing drag, reduction in parasite-drag area may result in increased weight whereas, in other cases, it does not. The final design, however, must be a compromise between the reduction of drag and the increase in weight .


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    Titel :

    Reduction of Helicopter Parasite Drag


    Beteiligte:

    Erscheinungsdatum :

    01.08.1954


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Reduction of helicopter parasite drag

    Harrington, R.D. | Engineering Index Backfile | 1954


    Reduction of helicopter parasite drag

    Harrington, Robert D. | TIBKAT | 1954


    Flight Researches on Reducing Helicopter Parasite Drag

    Akimov, A. / Vozhdaev, U. / Associazione Italiana di Aeronautica ed Astronautica et al. | British Library Conference Proceedings | 1993


    Parasite-Drag Measurements of Five Helicopter Rotor Hubs

    Churchill, Gary B. / Harrington, Robert D. | NTRS | 1959


    Parasite-drag measurements of five helicopter rotor hubs

    Churchill, G.B. / Harrington, R.D. | Engineering Index Backfile | 1959