A comparison of experimental and numerical studies performed on a low-pressure turbine blade cascade at high-speed conditions, low reynolds numbers and various turbulence intensities-Reference-Cited by-同舟云学术

A comparison of experimental and numerical studies performed on a low-pressure turbine blade cascade at high-speed conditions, low reynolds numbers and various turbulence intensities

Published:2013-09-12 Issue:5 Volume:22 Page:413-423
ISSN:1003-2169
Container-title:Journal of Thermal Science
language:en
Short-container-title:J. Therm. Sci.

Author:

Michalek Jan,Straka Petr

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Link

http://link.springer.com/content/pdf/10.1007/s11630-013-0643-9.pdf

Reference23 articles.

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2. Mayle R. E.,: The Role of Laminar-Turbulent Transition in Gas Turbine Engines, Journal of Turbomachinery, vol.113, pp. 509–537, (1991).

3. Walker G. J.: The Role of Laminar-Turbulent Transition in Gas Turbine Engines: A Discussion, J. of Turbomachinery,, vol.115, pp. 207–217, (1993).

4. Curtis E. M., Hodson H. P., Banieghbal M. R., Denton J. D., Howell R. J., Harvey N. W.: Development of Blade Profiles for Low-Pressure Turbine Applications, J. of Turbomachinery, vol. 119, pp. 531–538, (1997).

5. Haselbach, F. et al.: The Application of Ultra High Lift Blading in the BR715 LP Turbine, ASME Turbo Expo, New Orleans, Louisiana, USA, (2001).

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