An investigating the factors affecting the choice of an optimum aircraft electrical system it was found that quantitative information on many phases of system operation was lacking.


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    Title :

    Current and Temperature Rise in Aircraft Cables, Part I - Single Cables under Steady State Conditions


    Contributors:
    M. Schach (author)

    Publication date :

    1949


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Steady-state theory of towing cables

    Eames, M.C. | Engineering Index Backfile | 1968


    The Performance of Aircraft Control Cables Under Service Conditions

    M. B. Benoy / R. A. Fell / P. H. Townshend | NTIS | 1976


    Permissible current intensities in electric cables on aircraft

    Ruhlemann, E. | Engineering Index Backfile | 1948


    Developments in aircraft control cables

    Beed, C.F. | Engineering Index Backfile | 1941


    Dynamics of Cables Towed from Aircraft

    J. G. R. Hansen / S. A. Crist | NTIS | 1972