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 article by C.WILLIAMS, in Am Helicopter v 47 n 9 Aug 1957 p 11)


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    Title :

    X-14 VTOL airplane -- Design tool


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1958 Vertical takeoff



    Publication date :

    1958


    Size :

    18 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    X-14 VTOL airplane -- Design tool

    Williams, C. | Engineering Index Backfile | 1957


    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