Unsteady vortex breakdown behaviour over a pitching-rolling 70° delta wing

被引：0

作者：

Kowal, H.J. ^{[1
]}

Vakili, A.D. ^{[2
]}

机构：

[1] 14 Air Maintenance Squadron, 14 Wing Greenwood, Nova Scotta, Tullahoma, TN, United States

[2] Univ. of Tennessee Space Institute, Tullahoma, TN, United States

来源：

| 2000年 / CASI, Ottawa, Canada卷 / 46期

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引用

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[1] VORTEX BREAKDOWN OVER A PITCHING DELTA-WING
GURSUL, I
YANG, H
JOURNAL OF FLUIDS AND STRUCTURES, 1995, 9 (05) : 571 - 583
[2] Nonlinear response of vortex breakdown over a pitching delta wing
Menke, M
Gursul, I
JOURNAL OF AIRCRAFT, 1999, 36 (03): : 496 - 500
[3] Computational investigation into vortex breakdown over a pitching delta wing at supersonic speeds
Hadidoolabi, M.
Ansarian, H.
SCIENTIA IRANICA, 2017, 24 (06) : 2915 - 2928
[4] Computation of vortex breakdown on a rolling delta wing
Gordnier, R.E., 1600, American Institute of Aeronautics and Astronautics Inc. (32):
[5] Computational investigation of vortex structure and breakdown over a delta wing at supersonic pitching maneuver
Hadidoolabi, M.
Ansarian, H.
JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2018, 40 (02)
[6] Computational investigation of vortex structure and breakdown over a delta wing at supersonic pitching maneuver
M. Hadidoolabi
H. Ansarian
Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2018, 40
[7] ONSET OF VORTEX BREAKDOWN ABOVE A PITCHING DELTA-WING
VISBAL, MR
AIAA JOURNAL, 1994, 32 (08) : 1568 - 1575
[8] NUMERICAL ANALYSIS OF THE FLOW PATTERN AND VORTEX BREAKDOWN OVER A PITCHING DELTA WING AT SUPERSONIC SPEEDS
Hadidoolabi, M.
Ansarian, H.
JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2017, 58 (03) : 392 - 401
[9] Numerical analysis of the flow pattern and vortex breakdown over a pitching delta wing at supersonic speeds
M. Hadidoolabi
H. Ansarian
Journal of Applied Mechanics and Technical Physics, 2017, 58 : 392 - 401
[10] COMPUTATION OF VORTEX BREAKDOWN ON A ROLLING DELTA-WING
GORDNIER, RE
JOURNAL OF AIRCRAFT, 1995, 32 (03): : 686 - 688

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