Development of flow asymmetry over a 20-degree circular cone at low speed

Collection of Technical Papers - 37th AIAA Fluid Dynamics Conference

Volumn 2, Issue , 2007, Pages 1030-1067

  Meng, Xuanshi ^a   Jia, Chun ^a   Qiao, Zhide ^a   Gao, Chao ^a   Luo, Shijun ^b   Liu, Feng ^b,c  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b University of California at Irvine   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTINUOUS WAVE CURVE; FLOW ASYMMETRY; HYDRODYNAMIC INSTABILITY;

ANGLE OF ATTACK; CONES; CYLINDERS (SHAPES); PRESSURE DISTRIBUTION; REYNOLDS NUMBER; WIND TUNNELS;

FLOW PATTERNS;

EID: 35648951622     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Hunt, B. L., "Asymmetric vortex forces and wakes on slender bodies," AIAA Paper 1982-1336, Aug. 1982.
2. Ericsson, L. and Reding, J., "Asymmetric flow separation and vortex shedding on bodies of revolution," Tactical Missile Aerodynamics: General Topics, Progress in Astronautics and Aeronautics, edited by M. Hemsh, Vol. 141, American Institute of Aeronautics and Astronautics, New York, 1992, pp. 391-452.
3. Champigny, P., "Side forces at high angles of atack. Why, when, how?" La Recherche Aerospatiale, , No. 4, 1994, pp. 269-282.
4. Keener, E.R. and Chapman, G.T., "Similarity in vortex asymmetries over slender bodies and wings," AIAA Journal, Vol. 15, 1977, pp. 1370-1372.
5. Ericsson, L.E., "Source of high alpha vortex asymmetry at zero sideslip," Journal Aircraft, Vol. 29, 1992, pp. 1086-1090.
6. Coe, P., Chambers, J., and Letko, W., "Asymmetric lateral-directional characteristics of pointed bodies of revolution at high angle of attack," NASA TN D-7095, 1972.
7. Keener, E., Chapman, G., Cohen, L., and Taleghani, J., "Side forces on Forebodies at high angles of attack and Mach numbers from 0.1 to 0.7: two tangent ogives, paraboloid and cone," NASA TM X-3438, Feb. 1977.
8. Lowson, M.V., and Ponton, A.J.C., "Symmetric and asymmetric vortex flows at high angle of attack," AIAA Paper 1991-0276, Jan. 1991.
9. Fiddes, S., "Separated flow about cones at incidence-theory and experiment," Proceedings of Symposium on Studies of Vortex Dominated Flow, NASA/LRC, 1985, pp. 285-310.
10. Van Dyke, M., An Album of Fluid Motion, Photo 73, Parabolic Press, 1982.
11. Dyer, D. E., Fiddes, S. P., and Smith, J. H. B., "Asymmetric vortex formation from cones at incidence - a simple inviscid model," Aeronautical Quarterly, Vol. 31, 1982, pp. 293-312.
12. Pidd, M. and Smith, J., "Asymmetric vortex flow over circular cones," Vortex Flow Aerodynamics, AGARD CP-494, July 1991, pp. 18-1-11.
13. Cai, J., Liu, F., and Luo, S., "Stability of symmetric vortices in two-dimensions and over three-dimensional slender conical bodies," J. Fluid Mech., Vol. 480, April 2003, pp. 65-94.
14. Cai, J., Luo, S., and Liu, F., "Stability of Symmetric and asymmetric vortex pairs over slender conical wings and bodies," Physics of Fluids, Vol. 16, No. 2, Feb. 2004, pp. 424-432.
15. Hall, R.M., "Forebody and missile side forces and the time analogy," AIAA-87-0327, Jan. 1987
16. Hall, R.M., "Influence of Reynolds number on forebody side forces for 3.5-diameter tangent-ogive bodies," AIAA-87-2274, Jun. 1987
17. Lamont, P.J., "Pressure around an inclined ogive cylinder with laminar, transitional, or turbulent separation," AIAA Journal, Vol. 20, No. 11, Nov. 1982, pp. 1492-1499.
18. Keener, E.R., "Oil flow separation Patterns on an ogive forebody," AIAA Journal, Vol. 21, No. 4, Apr. 1983, pp. 550-556.
19. Jia, C., Meng, S., Qiao, Z., Gao, C., Luo, S., and Liu, F., "Pressure around a 20-degree circular cone at 35-degree angle of attack and low speed," AIAA Paper 2007-4453 Jun. 2007