Effects of angle of attack on wing rock motion induced by the flows over slender body with low swept wing
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy
Link
http://link.springer.com/content/pdf/10.1007/s11433-014-5630-y.pdf
Reference18 articles.
1. Katz J. Wing/vortex interactions and wing rock. Prog Aerosp Sci, 1999, 35: 727–750
2. Nelson R C, Pelletier A. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers. Prog Aerosp Sci, 2003, 39: 185–248
3. Brandon J M, Nguyen L T. Experimental study of effects of forebody geometry on high angle of attack stability. J Aircraft, 1988, 25: 591–597
4. Fratello D J, Croom M A, Nguyen L T, et al. Use of updated NASA langley radio-controlled drop-model technique for high-alpha studies of the X-29A configuration. AIAA Paper, 1987, AIAA-87-2559
5. Quast T, Nelson R C, Fisher D F. A study of high alpha dynamics and flow visualization for a 2.5% model of the F-18 HARV undergoing wing rock. AIAA Paper, 1991, AIAA-91-3267
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2. Effects of Reynolds Numbers on Wing Rock Induced by Forebody Vortices;AIAA Journal;2017-09
3. Unsteady analysis of six-DOF motion of a 6:1 prolate spheroid in viscous fluid;Science China Physics, Mechanics & Astronomy;2017-08-20
4. Fluid-structure interaction of a rolling restrained body of revolution at high angles of attack;Physics of Fluids;2017-03
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