Nonintrusive measurements of vortex flows on delta wings in a water tunnel
- 6 June 1988
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Leading edge vortex dynamics on a delta wing undergoing a wing rock motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Flow visualization of high angle of attack vortex wake structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Self-induced wing rock of slender delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Improved calculations of leading-edge separation from slender, thin, delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1968