Advantages due to use of controllable pitch; conditions which make its use essential; effect of altitude; take-off improvements of from 50 to 100% noticed in cases where throttle stop must be used when operating at sea level; cruising at altitude; fuel economy; engine cranking while flying; range of pitch; conclusions. Before Soc Automotive Engrs. (see also Aeroplane v 47 n 1218 Sept 26 1934 p 370-2)


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    Title :

    Effect of pitch control


    Additional title:

    West Flying


    Contributors:

    Published in:

    Western Flying ; 14 , n 7


    Publication date :

    1934


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Effect of pitch control

    Wright, T.P. | Engineering Index Backfile | 1934


    Pitch control

    Lombard, A.E. / Wright, T.P. | Engineering Index Backfile | 1933


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