Effect of coning motion and blowing on the asymmetric side forces on a slender forebody

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Zeiger, Matthew D ^a   Telionis, Demetri P ^a  

^a Virginia Polytechnic Institute and State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; VORTEX FLOW; WIND TUNNELS;

ANGLES OF ATTACK; AXIAL POSITIONS; CONING MOTION; LOW-SPEED WIND TUNNEL; MOTION EFFECT; RECOVERY TIME; VORTEX CONTROL; VORTEX PATTERN;

ANGLE OF ATTACK;

EID: 84983178100     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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2. Zeiger, M.D. and Telionis, D.P, "Vortex Asymmetry Over Ogive Cylinders in Coning and Pitching Motions," A1AA Paper 92-0206, Jan. 1996.
3. Skow, A.M., and Erickson, G.E., "Modern Fighter Aircraft Design for High Angle of Attack," AGARD Lecture Series № 121, High-Angle-of-Attack Aerodynamics, Mar. 1982.
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10. Alexan, K., Hanff, E.F., and Kind, R.J, "Water-Tunnel Investigation of Dynamic Manipulation of Forebody Vortices," AIAA Paper 94-0503, January 1994.
11. Roos, F.W., ""Microblowing" for High-Angle-of-Attack Vortex Flow Control on a Fighter Aircraft," AIAA Paper 96-0543, January 1996.
12. Williams, D. and Bernhardt, J., "Proportional Control of the Asymmetric Forebody Vortices with the Unsteady Bleed Technique," AIAA Paper 90-1629, June 1990.
13. Rediniotis, O.K., "The Transient Development of Vortices Over a Delta Wing," Ph.D. Dissertation, VPI& SU, Oct. 1992.
14. Schiff, L.B., and Tobak, M., "Results From a New Wind-Tunnel Apparatus for Studying Coning and Spinning Motions of Bodies of Revolution," AIAA Journal, Vol.8, № 11, Nov. 1970.
15. Yoshinaga, T., Tate, A. and Inoue, R.,"Coning Motion of Slender Bodies at High Angles of Attack in Low Speed Flow," AIAA Paper № SI.