Flowfield in the vicinity of an F/A-18 vertical fin at high angles of attack

被引：0

作者：

Lee, B.H.K. ^{[1
]}

Brown, D. ^{[1
]}

Tang, F.C. ^{[1
]}

Plosenski, M. ^{[1
]}

机构：

[1] Inst for Aerospace Research, Ottawa, Canada

来源：

Journal of Aircraft | 1993年 / 30卷 / 01期

关键词：

Military aircraft;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：69 / 74

共 35 条

[21] Investigation of the unsteady pressure fluctuations on an F/A-18 wing at high incidence
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[22] Investigation of the unsteady pressure fluctuations on an F/A-18 wing at high incidence
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J Aircr, 5 (888-894):
[23] VORTICAL FLOW STRUCTURE NEAR THE F/A-18 LEX AT HIGH-INCIDENCE
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[25] Tail buffet of F/A-18 at high incidence with sideslip and boil (Part 2)
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[27] Head positioning for high +Gz loads: An analysis of the techniques used by F/A-18 pilots
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[28] Numerical Study About Buffet Characteristics and Attenuation of Vertical Tail at High Angles of Attack
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[29] Numerical Study About Buffet Characteristics and Attenuation of Vertical Tail at High Angles of Attack
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International Journal of Aeronautical and Space Sciences, 2020, 21 : 315 - 328
[30] Use of high-fidelity simulation in the development of an F/A-18 active ground collision avoidance system
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SAE (Society of Automotive Engineers) Transactions, 1992, 101 (Sect 1):

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