Transonic flows around a carrying airfoil profile
β Scribed by Yu. B. Lifshits; O. S. Ryzhov
- Publisher
- Springer
- Year
- 1978
- Tongue
- English
- Weight
- 713 KB
- Volume
- 13
- Category
- Article
- ISSN
- 0015-4628
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π SIMILAR VOLUMES
A double-wedge with a relative thickness d/c > 0.15 forms a vortex street in its wake. This was investigated experimentally in the Mach number range of 0.4 to 0.75. The strength and the frequency of the pressure fluctuations which are produced by the vortices, were measured on the surface of the wed
## Abstract A time marching integral equation method has been proposed here which does not have the limitation of the time linearized integral equation method in that the latter method can not satisfactorily simulate the shock wave motions. Firstly, a model problemβone dimensional initial and bound