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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    Title :

    Ch-113 Crash Position Indicator Flight Trials


    Contributors:

    Publication date :

    1979


    Size :

    35 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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