In calculations described it is assumed that maximum braking thrust is coincident with plane speed of 150 km per hr; landing run with fraction brakes only and with braking by two propellers, but without friction braking employment of propeller braking by reversing pitch results in substantial shortening of land run. English Abstract from Rivista Aeronautica May/June 1946. (See also Engrs' Digest (Am Edition) v 3 n 9 Sept 1946 p 457-8)


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    Title :

    Length and time of landing run with airscrew-braking


    Additional title:

    Engrs' Digest (Brit Edition)


    Contributors:
    Grazi, S.R. (author)


    Publication date :

    1946


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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