Shock-induced secondary vortices on a delta wing - An Euler simulation

Current Science

Volumn 72, Issue 11, 1997, Pages 874-876

  Kumar, Anand ^a  

^a CSIR Centre for Mathematical Modelling and Computer Simulation   (India)

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Indexed keywords

EID: 23744498745     PISSN: 00113891     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

1. Hoeijmakers, H. W. M., Jacobs, J. M. J. W. and Van Den Berg, J. I., in Proceedings of the 17th International Council of the Aeronautical Sciences, 1990, vol. 1, pp. 486-499.
2. Bannink, W. J. and Houtman, E. M., in IUTAM Symposium on Fluid Dynamics of High Angles of Attack (eds Kawamura, R. and Aihara, Y.), Springer, Berlin, 1993, pp. 399-411.
3. Hitzel, S. M., 'Wing vortex flows up into vortex breakdown - A numerical simulation', AIAA Paper 88-2518, 1988.
4. Longo, J. M., Am. Inst. Aeronaut. Astronaut. J., 1995, 33, 680-687.
5. Kumar, A., Am. Inst. Aeronaut. Astronaut. J., 1996, 34, 2038-46.
6. Houtman, E. M. and Bannink, W. J., 'Experimental investigation of the transonic flow at the leeward side of a delta wing at high incidence', Report LR-518, TU Delft, 1987.
7. Elsenaar, A. and Hoeijmakers, H. W., 'An experimental study of the flow over a sharp-edged delta wing at subsonic and transonic speeds', AGARD CP-494, Paper No. 15, 1990.
8. Bickley, W. G., 'Critical conditions for compressible flow', ARC R&M No. 2330, 1950.