The passage toward stall of nonslender delta wings at low reynolds number

15th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2001, Pages

  Michael, V O L ^a   Gharibt, Morteza ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894411111     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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2. Shih, C, and Ding, Z. Unsteady Structure of Leading- Edge Vortex Flow over a Delta Wing. AIAA paper # 96-0664, January 1996.
3. Willert, C.E. Stereoscopic Digital Particle Image Velocimetry for Application in Wind Tunnel Flows. Meas. Sci. TechnoL, Vol. 8,1997, pp. 1465-1479.
4. Jobe, C.E. Vortex Breakdown Location over 65° Delta Wings - Empiricism and Experiment. AIAA paper 98-2526, June 1998
5. Willert, C.E., and Gharib, M. Digital Particle Image Velocimetry. Experiments in Fluids, Vol. 10, 1991. pp. 181-193.
6. Lawson, NJ., ad Wu, J. 'Three-Dimensional Particle Image Velocimetry: Experimental Error of a Digital Angular Stereoscopic System. Meas. Sci. Technol., 1997.
7. Miau, J.J., Kuo, K.T., Liu, W.H., Hsieh, S.J., Chou, J.H., and Lin, C.K. Flow Developments above 50-Deg Sweep Delta Wings with Different Leading-Edge Profiles. J. Aircraft, Vol. 32, No. 4, Jul-Aug 1995.
8. Earnshaw, P.B., and Lawford, J.A. Low-Speed Wind Tunnel Experiments on a Series of Sharp-Edged Delta Wings. Reports and Memorabilia, No. 3424, March 1964.
9. Ol, M. An Experimental Investigation of Leading Edge Vortices and Passage to Stall of Nonslender Delta Wings. RTO AVT-072, Symposium on Advanced Flow Management. May 2001.
10. Ol, M. The Passage Toward Stall of Nonslender Delta Wings at Low Reynolds Number. Ph.D. Thesis, Caltech, 2000.
11. Hall, M.G. A Theory for the Core of a Leading-Edge Vortex. JFM, Vol. 11. 1961, pp. 209-228.
12. Gad-el-Haq, M. and Blackwelder, R. F. 'The Discrete Vortices from a Delta Wing. AIAA Journal. Vol. 23, No. 6, June 1985, pp. 961-962.
13. Delery, J.M. Aspects of Vortex Breakdown. Prog. Aerospace Sci. Vol. 30, pp. 1-59, 1994.