DEVELOPMENT OF A TWIN-TURBOFAN V/STOL AIRCRAFT.

被引：0

|

作者：

Ciminera, Michael V.

机构：

来源：

Annual Forum Proceedings - American Helicopter Society | 1980年

关键词：

Compendex;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Aircraft, VTOL/STOL

引用

收藏

相关论文

共 50 条

[1] CONTROL OF V/STOL AIRCRAFT.
Franklin, J.A.
Aeronautical Journal, 1986, 90 (895): : 157 - 173
[2] AIRSPEED VECTOR SENSOR FOR V/STOL AIRCRAFT.
Durbin, Enoch
McGeer, Tad
1600, (19):
[3] Experimental V/STOL aircraft. Lessons learned
Lindenbaum, Bernie
Vertiflite, 1991, 37 (01):
[4] DISPLAYS FOR APPROACH AND LANDING OF V/STOL AIRCRAFT.
Rep
1600,
[5] DIGITAL ENGINE CONTROL FOR V/STOL AND V/TOL AIRCRAFT.
ANON
1982, V 54 (N 9): : 19 - 22
[6] THRUST MODULATION METHODS FOR A SUBSONIC V/STOL AIRCRAFT.
WOOLLETT, RICHARD R.
1981,
[7] PROPULSIVE WING TURBOFAN V/STOL
WINBORN, BR
SAE TRANSACTIONS, 1966, 74 : 89 - &
[8] V/STOL AIRCRAFT
不详
IEEE SPECTRUM, 1990, 27 (05) : 24 - 24
[9] ADVANCED CIRCULATION CONTROL WING SYSTEM FOR NAVY STOL AIRCRAFT.
Nichols Jr., James H.
Englar, Robert J.
AIAA Paper, 1980,
[10] CIRCULATION CONTROL TECHNOLOGY FOR POWERED-LIFT STOL AIRCRAFT.
Englar, Robert J.
Lockheed horizons, 1987, (24): : 44 - 55

← 1 2 3 4 5 →