Visualized vortices on unmanned combat air vehicle planform: Effect of reynolds number

Journal of Aircraft

Volumn 41, Issue 5, 2004, Pages 1244-1247

  Elkhoury, M ^a,b   Rockwell, D ^a,b  

^a LEHIGH UNIVERSITY   (United States)

^b Lehigh University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; CAMERAS; CHARGE COUPLED DEVICES; FLOW PATTERNS; FLOW VISUALIZATION; FUNCTIONS; FUSELAGES; LASER DOPPLER VELOCIMETERS; REYNOLDS NUMBER; UNMANNED VEHICLES; VORTEX FLOW; WINGS;

DELTA WINGS; DYE VISUALIZATION; PRESSURE COEFFICIENTS; SURFACE PRESSURE;

AERODYNAMICS;

EID: 7544242032     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.6290     Document Type: Article

References (6)

1. Hebbar, S. K., Platzer, M. F., and Fritzelas, A. E., "Reynolds Number Effects on the Vortical-Flow Structure Generated by a Double-Delta Wing," Experiments in Fluids, Vol. 28, 2000, pp. 206-216.
2. Verhaagen, N. G., "Effects of Reynolds Number on Flow over 76/40-Degree Double-Delta Wings," Journal of Aircraft, Vol. 39, No. 6, 2002, pp. 1045-1052.
3. Visser, K. D., and Washburn, A. E., "Transition Behavior on Flat Plate Delta Wings," AIAA Paper 94-1850, June 1994.
4. Verhaagen, N. G., Jenkins, L. N., Kern, S. B., and Washburn, A. E., "A Study of the Vortex Flow over a 76/40-deg Double-Delta Wing," AIAA Paper 95-0650, Jan. 1995.
5. Gordnier, R. E., and Visbal, M. R., "Higher-Order Compact Difference Scheme Applied to the Simulation of a Low Sweep Delta Wing Flow," AIAA Paper 2003-0620, Jan. 2003.
6. Yaniktepe, B., and Rockwell, D., "Flow Structure in Regions of Vortex Breakdown and Stall on a Delta Wing of Low Sweep Angle," AIAA Journal, Vol. 42, No. 3, 2004, pp. 513-523.