CAA War Training Service has been operating fleet of several thousand light commercial airplanes of from 50 to 450 hp on intensive pilot training program; some of difficulties encountered with operation and maintenance of present day light airplane of between 50 to 75 hp are pointed out as revealed by review of reports submitted; re sume of most prominent difficulties presented by components. Before Inst Aeronautical Sciences.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural design problems of light aircraft


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1945


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Unique structural problems in supersonic aircraft design

    Michell, F.P. | Engineering Index Backfile | 1956


    Practical Structural Design Problems of Supersonic Aircraft

    Heath, W.G. / Heath, B.O. | Emerald Group Publishing | 1957


    Practical structural design problems of supersonic aircraft

    Heath, W.G. / Heath, B.O. | Engineering Index Backfile | 1957


    Trends in Light Aircraft Structural Design

    Gerteis, Jerry H. / Dussault, John C. | SAE Technical Papers | 1961


    Trends in light aircraft structural design

    Gerteis, J.H. / Dussalt, J.C. | Engineering Index Backfile | 1961