Measurement and prediction of the noise of the harrier V/STOL aircraft

被引：0

|

作者：

Berry, B.B.

Harris, A.L.

Payne, R.C.

Milton, N.E.

机构：

来源：

Proceedings - International Conference on Noise Control Engineering | 1988年

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

收藏

相关论文

共 50 条

[41] DIGITAL ENGINE CONTROL FOR V/STOL AND V/TOL AIRCRAFT.
ANON
1982, V 54 (N 9): : 19 - 22
[42] DESIGNING A V/STOL FIGHTER - MCDONNELLS AV-8B HARRIER-II
DEMEIS, R
AEROSPACE AMERICA, 1985, 23 (05) : 88 - 91
[43] THRUST MODULATION METHODS FOR A SUBSONIC V/STOL AIRCRAFT.
WOOLLETT, RICHARD R.
1981,
[44] WIND TUNNEL TEST CONSIDERATIONS UNIQUE TO V/STOL AIRCRAFT
BLACK, EL
SAE TRANSACTIONS, 1968, 77 : 108 - &
[45] SIMULATION EVALUATION OF AN ADVANCED CONTROL CONCEPT FOR A V/STOL AIRCRAFT
MORALEZ, E
MERRICK, VK
SCHROEDER, JA
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1989, 12 (03) : 334 - 341
[46] TECHNICAL PROBLEMS IN CONCEPTION AND UTILISATION OF V/STOL TRANSPORT AIRCRAFT
WILLIAMS, J
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1969, 17 (11): : 369 - &
[47] Robust control of transition maneuvers for a class of V/STOL aircraft
Naldi, Roberto
Marconi, Lorenzo
AUTOMATICA, 2013, 49 (06) : 1693 - 1704
[48] LIFT FAN PROPULSION SYSTEMS - V/STOL AIRCRAFT CONTROL
BEELER, EF
VOLK, LJ
SAE TRANSACTIONS, 1966, 74 : 159 - &
[49] SOME CONSIDERATIONS OF DIRECT-LIFT V/STOL AIRCRAFT
KATZENBERGER, EF
ULISNIK, HD
ADLER, A
ANNALS OF THE NEW YORK ACADEMY OF SCIENCES, 1963, 107 (01) : 380 - &
[50] ZERO-LENGTH INLETS FOR SUBSONIC V/STOL AIRCRAFT
GLASGOW, ER
BECK, WE
WOOLLETT, RR
JOURNAL OF AIRCRAFT, 1983, 20 (05): : 397 - 403

← 1 2 3 4 5 →