essential to gain knowledge of the interaction between the jet and cross flow and to develop a new film-cooling Effects of the computational time step and grid stretching on numerical solutions of a two-dimensional laminar boundary layer technology with a higher efficiency. with a planar jet inject
Simulation of the near field of a jet in a cross flow
โ Scribed by Murray Rudman
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 808 KB
- Volume
- 12
- Category
- Article
- ISSN
- 0894-1777
No coin nor oath required. For personal study only.
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