Influence of the aspect ratio on the aerodynamics of the delta wing at high angle of attack

被引：0

作者：

Er-El, J. ^{[1
]}

Zohar, Y. ^{[1
]}

机构：

[1] Technion-Israel Inst of Technology, Israel

来源：

| 1600年 / 25期

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[21] Low-aspect-ratio wing aerodynamics at low reynolds numbers
Torres, GE
Mueller, TJ
AIAA JOURNAL, 2004, 42 (05) : 865 - 873
[22] Effects of angle of attack on nonlinear flutter of a delta wing
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AIAA JOURNAL, 2001, 39 (01) : 15 - 21
[23] Low-aspect-ratio wing aerodynamics at low reynolds numbers
Torres, G.E., 1600, American Inst. Aeronautics and Astronautics Inc. (42):
[24] HIGH ANGLE-OF-ATTACK HYPERSONIC AERODYNAMICS
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JOURNAL OF SPACECRAFT AND ROCKETS, 1988, 25 (05) : 343 - 344
[25] AERODYNAMICS OF FINNED MISSILES AT HIGH ANGLE OF ATTACK
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[26] Simulation of the Influence of Aspect Ratio on the Aerodynamics of Rectangular Prisms
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[27] High angle-of-attack aerodynamics of a straight wing with finite span using a discrete vortex method
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[28] Unsteady aerodynamic characteristics of a delta wing oscillating in pitch to very high angle of attack
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[29] Investigation of effect of suction on delta wing separation flow at high angle-of-attack
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[30] Numerical simulation of full-span delta wing buffet at high angle of attack
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