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)
X-14 VTOL airplane -- Design tool
Am Helicopter
American Helicopter ; 47 , n 9
1957
Article (Journal)
English
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X-14 VTOL airplane -- Design tool
Engineering Index Backfile | 1958
|THE X-14 VTOL AIRPLANE - A DESIGN TOOL
SAE Technical Papers | 1958
|Design aspects of bell aircraft VTOL airplane
Engineering Index Backfile | 1955
|Design aspects of bell aircraft VTOL airplane
Engineering Index Backfile | 1955
|VTOL Airplane Control in Transition Regimes
NTIS | 1974
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