Control of asymmetric vortical flows over delta wings at high angles of attack

Journal of Aircraft

Volumn 27, Issue 5, 1990, Pages 429-435

  Wood, N J ^a,b   Roberts, L ^a   Celik, Z ^a  

^a STANFORD UNIVERSITY   (United States)

^b UNIVERSITY OF BATH   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS--VORTEX FLOW; STRAIN GAGES--APPLICATIONS;

ASYMMETRIC VORTICAL FLOWS; DELTA WING VORTICAL FLOW; HIGH ANGLES OF ATTACK FLOW FIELDS; STRAIN GAUGE BALANCE MEASUREMENTS;

AIRCRAFT;

EID: 0025430383     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.25294     Document Type: Article

References (16)

1. 'Herbst, W. B., "Dynamics of Air Combat," Journal of Aircraft, Vol. 20, No. 7, 1983, pp. 594-594.
2. Scott, W. B., "NASA Adds to Understanding of High Angle of Attack Regime," Aviation Week and Space Technology, May 22, 1989, pp. 36-42.
3. Chody, J. R., Hodginson, J., and Skow, A. M., "Combat Aircraft Control Requirements for Agility," AGARD Symposium on Combat Aircraft Controls and of Ground Effects, Oct. 1989.
4. Levin, D., and Katz, J., "Dynamic Load Measurement with Delta Wings Undergoing Self-Induced Roll Oscillations," Journal of Aircraft, Vol. 21, No. 1, 1984, pp. 30-36.
5. Jean Ross, A., and Nguyen, L. T., "Some Observations Regarding Wing Rock Oscillations at High Angles of Attack," AIAA Paper 88-4371, Aug. 1988.
6. Jun, Y.W., and Nelson, R. C., "Leading Edge Vortex Dynamics on a Delta Wing Undergoing a Wing Rock Motion," AIAA Paper 87-0332, Jan. 1987.
7. 'Ericsson, L. E., "The Fluid Mechanics of Slender Wing Rock," Journal of A ircraft, Vol. 21, No. 5, 1984, pp. 322-328.
8. Hess, R. A., "Recent Results in the Identification of High Angle of Attack F/TF-18 Aerodynamics," AIAA Paper 88-4348, Aug. 1988.
9. Kandebo, S. W., "Modified F-15B to Demonstrate STOL, Maneuver Capability," Aviation Week and Space Technology, May 29, 1989, pp. 44-47.
10. Kandebo, S. W., "Second X-29 Will Execute High-Angle-of-Attack Flights," Aviation Week and Space Technology, Oct. 31, 1988, pp. 36-38.
11. Ashley, H., and Clarke, L., "On the Feasibility of Low Speed Fighter Maneuvers Involving Extreme Angles of Attack," Stanford Univ., Stanford, CA, Rept. SUDAAR 563, July 1987.
12. Wood, N. J., and Roberts, L., "Control of Vortical Lift on Delta Wings by Tangential Leading Edge Blowing," Journal of Aircraft, Vol. 25, No. 3, 1988, pp. 236-243.
13. Yeh, D. T., Tavelia, D. A., and Roberts, L., "Numerical Study of the Effect of Tangential Leading Edge Blowing on Delta Wing Vortical Flow," AIAA Paper 89-0341, Jan. 1989.
14. Wood, N. J., and Roberts, L., "The Control of Delta Wing Aerodynamics at High Angles of Attack," Royal Aeronautical Society Conference on the Control and Exploitation of Separated Flows, London, April 1989.
15. Ward, D. T., and Stout, L. J., "Use of Differential Leading Edge Flaps for Lateral Control at High Angle of Attack," AIAA Paper 86-0168, Jan. 1986.
16. Wood, N. J., Roberts, L. and Lee, K. T., "The Control of Vortical Flow on a Delta Wing at High Angles of Attack," AIAA Paper 87-2278, Aug. 1987.