Results of recent experimental studies into the effect of compressibility on dynamic stall of oscillating airfoils are reviewed. Stroboscopic schlieren images of the strongly unsteady flow field are presented, showing the development of the dynamic stall vortex, and its progression down the airfoil.
โฆ LIBER โฆ
The Effect of Pitch Location on Dynamic Stall
โ Scribed by Jumper, E. J.; Dimmick, R. L.; Allaire, A. J. S.
- Book ID
- 125459388
- Publisher
- The American Society of Mechanical Engineers
- Year
- 1989
- Tongue
- English
- Weight
- 711 KB
- Volume
- 111
- Category
- Article
- ISSN
- 0098-2202
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