Design of a small supersonic oblique-wing transport aircraft

被引：0

作者：

机构：

[1] van der Velden, Alexander J.M.

[2] Torenbeek, Egbert

来源：

van der Velden, Alexander J.M. | 1600年 / 26期

关键词：

(Edited Abstract);

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

共 50 条

[21] Dynamic characteristics analysis and flight control design for oblique wing aircraft
Wang Lixin
Xu Zijian
Yue Ting
CHINESE JOURNAL OF AERONAUTICS, 2016, 29 (06) : 1664 - 1672
[22] Dynamic characteristics analysis and flight control design for oblique wing aircraft
Yue, Ting (yueting_buaa@sina.com), 1664, Chinese Journal of Aeronautics (29):
[23] Dynamic characteristics analysis and flight control design for oblique wing aircraft
Wang Lixin
Xu Zijian
Yue Ting
Chinese Journal of Aeronautics, 2016, 29 (06) : 1664 - 1672
[24] OBLIQUE WING READY FOR RESEARCH AIRCRAFT
GREGORY, T
AEROSPACE AMERICA, 1985, 23 (06) : 78 - 81
[25] MULTIDISCIPLINARY DESIGN INTEGRATION METHODOLOGY FOR A SUPERSONIC TRANSPORT AIRCRAFT
DOVI, AR
WRENN, GA
BARTHELEMY, JFM
COEN, PG
HALL, LE
JOURNAL OF AIRCRAFT, 1995, 32 (02): : 290 - 296
[26] Multidisciplinary design integration methodology for a supersonic transport aircraft
Interdisciplinary Research Methods, Hampton, United States
J Aircr, 2 (290-296):
[27] STABILITY OF SWIVEL WING SUPERSONIC AIRCRAFT
BENNETCLARK, HC
NATURE, 1972, 239 (5373) : 451 - +
[28] Fatigue strength estimates for composite wing panels of prospective supersonic transport aircraft
Strizhius V.E.
Turbin N.V.
Aerospace Systems, 2024, 7 (01) : 75 - 81
[29] THE FLYING WING SUPERSONIC TRANSPORT
JONES, RT
AERONAUTICAL JOURNAL, 1991, 95 (943): : 103 - 106
[30] SPIN-TUNNEL INVESTIGATION OF A 1/13-SCALE MODEL OF THE NASA AD-1 OBLIQUE-WING RESEARCH AIRCRAFT.
White, William L.
Bowman Jr., James S.
NASA Technical Memorandum, 1982, : 1 - 26

← 1 2 3 4 5 →