Background of original air test vehicle and development of USAF research aircraft of horizontal attitude type, by Bell Aircraft Corp; two power plants are Armstrong-Siddeley "Viper" engines, possessing rated 150-hr life; ground pressure and ground heating effects; thrust diverter development; STOL and conventional flight performance; stability and control; future potential; wing span 34 ft, length 25 ft. (See also Soc Automotive Engrs -- Paper n 95B for meeting Sept 29-Oct 4 1958 18 p)


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    Title :

    X-14 VTOL airplane -- Design tool


    Additional title:

    Am Helicopter


    Contributors:

    Published in:

    Publication date :

    1957


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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


    Design aspects of bell aircraft VTOL airplane

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


    Design aspects of bell aircraft VTOL airplane

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


    VTOL Airplane Control in Transition Regimes

    A. P. Pashchenko | NTIS | 1974