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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    Titel :

    Length and time of landing run with airscrew-braking


    Weitere Titelangaben:

    Engrs' Digest (Brit Edition)


    Beteiligte:
    Grazi, S.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1946


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Airscrew braking

    Engineering Index Backfile | 1945


    Airscrew design

    Engineering Index Backfile | 1932


    Airscrew weight

    Gillmore, K.B. / Cleaver, A.V. | Engineering Index Backfile | 1941


    Selecting airscrew

    von Baumhauer, A.G. | Engineering Index Backfile | 1939


    Airscrew development

    Watts, H.C. | Engineering Index Backfile | 1936