A computational study of a canonical pitch-up, pitch-down wing maneuver

39th AIAA Fluid Dynamics Conference

Volumn , Issue , 2009, Pages

  Eldredge, Jeff D ^a   Wang, Chengjie ^a   Ol, Michael V ^b  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CANONICAL PROBLEMS; COMPUTATIONAL STUDIES; ELLIPTICAL WING; EXPERIMENTAL STUDIES; FLAT PLATE; FORCE GENERATION; LEADING EDGE; LEADING-EDGE VORTICES; PITCH RATE; SURFACE PRESSURE DISTRIBUTION; UNIFORM FLOW; VORTICITY FIELD; WAKE VORTEX; WING PROFILES;

DRAG; FLUID DYNAMICS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; VORTICITY; WAKES;

VORTEX FLOW;

EID: 78349295313     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. OL, M. V., "The High-Frequency, High-Amplitude Pitch Problem: Airfoils, Plates and Wings," AIAA Paper 2009-3686.
2. McCroskey, W. J., "Unsteady airfoils," Ann. Rev. Fluid Mech, Vol. 14, 1982, pp. 285-311.
3. Visbal, M. R. and Shang, J. S., "Investigation of the Flow Structure Around a Rapidly Pitching Airfoil," AIAA J., Vol. 27, No. 8, 1989, pp. 1044-1051.
4. Visbal, M. R., "Dynamic Stall of a Constant-Rate Pitching Airfoil," J. Aircraft, Vol. 27, No. 5, 1990, pp. 400-407.
5. McGowan, G. Z., Gopalarathnam, A., OL, M. V., and Edwards, J. R., "AIAA Paper 2009-0535, ".
6. OL, M. V., Dong, H., and Webb, C., "Motion Kinematics vs. Angle of Attack Effects in High-Frequency Airfoil Pitch/Plunge," AIAA Paper 2008-3822.
7. Eldredge, J. D., "Numerical simulation of the fluid dynamics of 2D rigid body motion with the vortex particle method," J. Comput. Phys., Vol. 221, 2007, pp. 626-648.