Numerical simulation of boundary-layer transition at Mach two
โ Scribed by Sandham, N. D. ;Adams, N. A.
- Publisher
- Springer
- Year
- 1993
- Tongue
- English
- Weight
- 306 KB
- Volume
- 51
- Category
- Article
- ISSN
- 0003-6994
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
The three-dimensional inviscid-viscous interaction generated by the intersection of an oblique shock with a turbulent boundary layer is examined theoretically. An incoming Mach 4 equilibrium turbulent boundary layer at Reynolds number Re~ = 2 ร 105 interacts with an oblique shock formed by a 16 ยฐ sh
Direct numerical simulation (DNS) has become a powerful tool in studying fundamental phenomena of laminar-turbulent transition of high-speed boundary layers. Previous DNS studies of supersonic and hypersonic boundary layer transition have been limited to perfect-gas flow over flat-plate boundary lay
In transitional and turbulent high speed boundary-layer flows the wall thermal boundary conditions play an important role and in many cases an assumption of a constant temperature or a specified heat flux may not be appropriate for numerical simulations. In this paper we extend a formulation for dir