Method laminar-turbulent transition control of supersonic boundary layer on a swept wing
โ Scribed by N. V. Semionov; A. D. Kosinov
- Book ID
- 110194284
- Publisher
- International Academic Publishing Co (Nauka/Interperiodica)
- Year
- 2007
- Tongue
- English
- Weight
- 120 KB
- Volume
- 14
- Category
- Article
- ISSN
- 0869-8643
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
The origins of turbulent ?ow and the transition from laminar to turbulent ?ow are the most important unsolved problems of ?uid mechanics and aerodynamics. - sides being a fundamental question of ?uid mechanics, there are numerous app- cations relying on information regarding transition location and
The eects of mean ยฏow three-dimensionality on the turbulent structure of the boundary layer on a swept wing are investigated experimentally. The conยฎguration of the test model used to simulate the inยฎnite swept wing condition is similar to that used by Van den Berg, B., Elsenaar, A., Lindhout, J.P.F