The development of the wake flowfield behind a symmetric cascade of finite-thickness flat plates in steady two-dimensional laminar incompressible flow is investigated for a wide range of Reynolds number. A spectral method is used to obtain the solution to a low-Reynolds-number expansion of the Navie
Laminar jet in “narrow” slot at large Reynolds numbers
✍ Scribed by V. E. Nakoryakov; I. N. Yaichnikova
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 1986
- Tongue
- English
- Weight
- 313 KB
- Volume
- 26
- Category
- Article
- ISSN
- 0021-8944
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