Tests were performed on the crash position indicator (CPI) installed on a CF CH-113 Labrador aircraft to determine the safe deployment envelope and the effect of CPI fitment on the flying qualities of the CH-113. The tuft predictions of CPI airfoil separation and trajectory were validated.


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    Titel :

    Ch-113 Crash Position Indicator Flight Trials


    Beteiligte:
    K. D. Nelson (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    35 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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