Pressure around a 20-degree circular cone at 35-degree angle of attack and low speed

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 3, Issue , 2007, Pages 2044-2109

  Jia, Chun ^a   Meng, Xuanshi ^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

BOUNDARY LAYER FLOW; MATHEMATICAL MODELS; PRESSURE DISTRIBUTION; PRESSURE MEASUREMENT;

ROLL ANGLES; SEMI-APEX ANGLES; SIDE-FORCE COEFFICIENT;

TURBULENT FLOW;

EID: 35649001922     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-4453     Document Type: Conference Paper

References (17)

1. Allen, H.J., and Perkins, E.W., "Characteristics of flow over inclined bodies of revolution," NACA RM-A50L07, 1951.
2. Keener, E.R. and Chapman, G.T., "Similarity in vortex asymmetries over slender bodies and wings," AIAA Journal, Vol. 15, 1977, pp. 1370-1372.
3. Ericsson, L.E., "Source of high alpha vortex asymmetry at zero sideslip," Journal Aircraft, Vol. 29, 1992, pp. 1086-1090.
4. 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.
5. 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.
6. 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.
7. Luo, S., "Asymmetric vortex flow over slender bodies," Proceedings of Conference on New Century Mechanics, Beijing, Nov. 2001, pp. 198-205.
8. Van Dyke, M., An Album of Fluid Motion, Photo 73, Parabolic Press, 1982.
9. 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.
10. Pidd, M. and Smith, J., "Asymmetric vortex flow over circular cones," Vortex Flow Aerodynamics, AGARD CP-494, July 1991, pp. 18-1-11.
11. 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.
12. 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.
13. Meng, S., Jia, C., Qiao, Z., Gao, C., Luo, S., and Liu, F., "Development of flow asymmetry over a 20-degree circular cone at low speed," AIAA Paper 2007-4118, June 2007 Miami, Fl.
14. Hall, R.M., "Forebody and missile side forces and the time analogy," AIAA-87-0327, Jan. 1987
15. Hall, R.M., "Influence of Reynolds number on forebody side forces for 3.5-diameter tangent-ogive bodies," AIAA-87-2274, Jun. 1987
16. 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.
17. Keener, E.R., "Oil flow separation patterns on an ogive forebody," AIAA Journal, Vol. 21, No. 4, Apr. 1983, pp. 550-556.