Interaction of missile nose-tip vortices with a control surface

AIAA Journal

Volumn 34, Issue 5, 1996, Pages 999-1006

  Kiedaisch, John W ^a,b   Acharya, Mukund ^a,b  

^a ILLINOIS INSTITUTE OF TECHNOLOGY   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

FLOW FIELDS; INTERACTION; MISSILES; NOSE TIP VORTICES; VORTICES;

EID: 0029656838     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13179     Document Type: Article

References (6)

1. Mendenhall, M. R., and Perkins, S. C., Jr., "Vortex Induced Characteristics of Missiles in Unsteady Maneuvers," AIAA Paper 89-0344, Jan. 1989.
2. Washburn, A. E., Jenkins, L. N., and Ferman, M. A., "Experimental Investigation of Vortex-Fin Interaction," AIAA Paper 93-0050, Jan. 1993.
3. Bodstein, G. C. R., George, A. R., and Hui, C. Y., "Vortex/Surface Interaction," AIAA Paper 93-0863, Jan. 1993.
4. Ericsson, L. E., and Reding, J. P., "Asymmetric Vortex Shedding from Bodies of Revolution," Tactical Missile Aerodynamics, edited by M. J. Hemsch and J. N. Nielsen, Vol. 104, Progress in Astronautics and Aeronautics, AIAA, New York, 1986, pp. 243-296.
5. Acharya, M., Kiedaisch, J., and Mohammad Hassan, M., "Asymmetric Vortical Flows Over Slender Bodies with Appendages," IIT Fluid Dynamics Research Center, TR, Chicago, IL, June 1994.
6. Kiedaisch, J. W., "Experimental Investigation of the Interaction of Missile Tip Vortices with a Control Surface," M.S. Thesis, Mechanical and Aerospace Engineering Dept., Illinois Inst. of Technology, Chicago, IL, 1994.