Roll-yaw control at high angle of attack by forebody tangential blowing

Journal of Aircraft

Volumn 35, Issue 1, 1998, Pages 69-77

  Pedreiro, Nelson ^a,c   Rock, Stephen M ^b,d,e   Celik, Zeki Z ^b,d,e   Roberts, Leonard ^b,d,e  

^a EMBRAER S A   (Brazil)

^b STANFORD UNIVERSITY   (United States)

^c 496 Lomita Mall   (United States)

^d Dept of Aero and Astronautics ^*

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; CLOSED LOOP CONTROL SYSTEMS; DELTA WING AIRCRAFT; FUSELAGES; MOTION CONTROL; UNSTEADY FLOW; WIND TUNNELS;

ANGLE OF ATTACK; FOREBODY TANGENTIAL BLOWING; ROLL YAW CONTROL;

WINGS;

EID: 0031655513     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2261     Document Type: Article

References (17)

1. Ericsson, L. E., and Reding, J. P., "Alleviation of Vortex Induced Asymmetric Loads," Journal of Spacecraft and Rockers, Vol 17, No. 6, 1980, pp. 546-553.
2. Rao, D. M., Moskovitz, C., and Murri, D. G., "Forebody Vortex Management for Yaw Control at High Angles of Attack," Journal of Aircraft, Vol. 24, No. 4, 1987, pp. 248-254.
3. Skow, A. M., Moore, W. A., and Lorincz, D. J., Forebody Vortex Blowing - A Novel Control Concept to Enhance Departure/Spin Recovery Characteristics of Fighter and Trainer Aircraft, CP-262, AGARD, No. 24, 1979, pp. 24-1-24-17.
4. Wong, G. S., Rock, S. M., Wood, N. J., and Roberts, L., "Active Control of Wing Rock Using Tangential Leading-Edge Blowing," Journal of Aircraft, Vol. 31, No. 3, 1994, pp. 659-665.
5. Alexan, K., Hanff, E. S., and Kind, R. J., "Water-Tunnel Investigation of Dynamic Manipulation of Forebody Vortices," AIAA Paper 94-0503, Jan. 1994.
6. Celik, Z. Z., and Roberts, L., "Vortical Flow Control on a Wing-Body Combination Using Tangential Blowing," AIAA Paper 92-4430, Aug. 1992.
7. Celik, Z. Z., Roberts, L., and Pedreiro, N., "The Control of Wing Rock by Forebody Blowing," AIAA Paper 93-3685, Aug. 1993.
8. Celik, Z. Z., Roberts, L., and Pedreiro, N., "Dynamic Roll and Yaw Control by Tangential Forebody Blowing," AIAA Paper 94-1853, June 1994.
9. Adams, R. J., Buffington, J. M., and Banda, S. S., "Active Vortex Flow Control for VISTA F-16 Envelope Expansion," AIAA Paper 94-3681, Aug. 1994.
10. Pedreiro, N., "Development of an Apparatus for Wind Tunnel Dynamic Experiments at High-α," NASA Joint Inst. for Aeronautics and Acoustics, TR-119, Stanford Univ., Stanford, CA, Feb. 1997.
11. Pedreiro, N., "Experiments in Aircraft Roll-Yaw Control Using Forebody Tangential Blowing," Ph.D. Dissertation, Aeronautics and Astronautics Dept., Stanford Univ., Stanford, CA, 1997.
12. Degani, D., "Numerical Investigation of the Origin of Vortex Asymmetry," AIAA Paper 90-0593, Jan. 1990.
13. Grismer, D. S., and Jenkins, J. E., "Critical-State Transients for a Rolling 65-Degree Delta Wing," Journal of Aircraft, Vol. 34, No. 3, 1997, pp. 380-386.
14. Jenkins, J. E., Myatt, J. H., and Hanff, E. S., "Body-Axis Rolling Motion Critical States of a 65-Degree Delta Wing," Journal of Aircraft, Vol. 33, No. 2, 1996, pp. 268-278.
15. Ericsson, L. E., and Hanff, E. S., "Further Analysis of High-Rate Rolling Experiments of a 65-Degree Delta Wing," Journal of Aircraft, Vol. 31, No. 6, 1994, pp. 1350-1357.
16. Tobak, M., and Chapman, G. T., "Nonlinear Problems in Flight Dynamics Involving Aerodynamic Bifurcations," AGARD Symposium on Unsteady Aerodynamics - Fundamentals and Applications to Aircraft Dynamics, CP-386, AGARD, 1985, pp. 25-1-25-15.
17. Kroo, I., and Roberts, L., "Forebody Tangential Blowing for Control at High Angles of Attack - Feasibility Study Final Report," NASA Joint Inst. for Aeronautics and Acoustics, TR-101, Stanford Univ., Stanford, CA, June 1991.