Measurements of a blown zero-pressure gradient boundary layer

Author:

Aly S. E.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering

Reference7 articles.

1. Sarippali, K. R.; Simpson, R. L.: Measurements of a zero-pressure, gradient boundary layer blown by an asymmetric jet. AIAA J. 23 (1985) 490–491

2. Goldstein, R. J.; Eckert, E. G.; Erikson, V. L.; Ramsey, J. W.: Film cooling following injection through inclined circular tubes. NASA CR 72612 (1969)

3. Jubran, B.; Brown, A.: Film cooling from two rows of holes inclined to the streamwise and spanwise directions. J. Engng. Gas Turbines Power 107 (1985) 84–91

4. Brown, A.; Saluja, C.: Film cooling from a single hole and a row of holes of variable pitch to diameter ratio. Int. J. Heat Mass Transfer 22 (1979) 525–533

5. Foster, R.; Haji-Sheikh, A.: An experimental investigation of boundary layer and heat transfer in the region of separated flow downstream of normal injection slots. J. Heat Transfer, Trans. ASME (1975) 260–266

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Injection effect on two dimensional boundary layer;Energy Conversion and Management;2000-04

2. Heat transfer — a review of 1992 literature;International Journal of Heat and Mass Transfer;1994-06

3. Study of a zero-pressure gradient boundary layer blown at low injection ratios;Energy Conversion and Management;1993-07

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