THRUST MODULATION METHODS FOR A SUBSONIC V/STOL AIRCRAFT.

被引：0
|
作者：
WOOLLETT, RICHARD R.
机构：
来源：
| 1981年
关键词：
D O I：
暂无
中图分类号：
V27 [各类型航空器]; V24 [航空仪表、航空设备、飞行控制与导航];
学科分类号：
082503 ;
摘要：
THE PAPER EXAMINES THE THRUST MODULATION RANGE, THRUST LEVEL, AND BLADE STRESSES FOR EACH OF THE THRUST MODULATION SYSTEMS. RESULTS WILL BE SHOWN AT THE HIGH ANGLES OF ATTACK ASSOCIATED WITH TILT-NACELLE V/STOL AIRCRAFT. FINALLY, THE INTERRELATIONSHIP BETWEEN THE INLET AND THE THRUST MODULATION SYSTEM ARE ILLUSTRATED FOR TWO INLET TYPES.
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