Baynes indicator comprises normal ASI with additional red pointer which is set at known steady flight stalling speed; this pointer is operated by mechanism inside instrument which will turn pointer to degree proportional to square root of G, so that correct stalling speed appropriate to prevailing G will be shown on dial, and margin between two pointers will thus represent speed range available between prevailing stalling and flying speed.


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    Title :

    Speed-range indicator


    Additional title:

    Flight


    Published in:

    Flight ; 48 , n 1907


    Publication date :

    1945


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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