Aspects of airplane equipped with Schweizer glider fuselage and empennage, modified Cessna wing, Bell helicopter landing skid, two Fairchild J-44 jet engines and Turbomeca Palouste turbocompressor; test vehicle is capable of hovering, translating at speeds required for transition and flying as airplane. (See also Can Aeronautical J v 1 n 4 Sept 1955 p 100-2)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Design aspects of bell aircraft VTOL airplane


    Additional title:

    Engineering


    Contributors:

    Published in:

    Engineering ; 179 , n 4663


    Publication date :

    1955


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Design aspects of bell aircraft VTOL airplane

    O'Malley, Jr., J.A. | Engineering Index Backfile | 1955


    X-14 VTOL airplane -- Design tool

    Williams, C. | Engineering Index Backfile | 1957


    X-14 VTOL airplane -- Design tool

    O'Malley, Jr., J.A. | Engineering Index Backfile | 1958


    THE X-14 VTOL AIRPLANE - A DESIGN TOOL

    O’MALLEY, JAMES A. / LANDPHAIR, LEE C. | SAE Technical Papers | 1958


    VTOL Airplane Control in Transition Regimes

    A. P. Pashchenko | NTIS | 1974