Comparisons Between Triggered Turbulent Spots and Unsteady Transition Phenomena on Compressor and Turbine Blading-Reference-Cited by-同舟云学术

Comparisons Between Triggered Turbulent Spots and Unsteady Transition Phenomena on Compressor and Turbine Blading

Published:2000 Issue: Volume: Page:365-370
ISSN:
Container-title:Laminar-Turbulent Transition
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Author:

Gostelow J. P.,Hodson H. P.,Walker G. J.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-662-03997-7_54

Reference7 articles.

1. Gostelow JP, Melwani N, Walker GJ (1996): Effects of streamwise pressure gradient on turbulent spot development. ASME Journal of Turbomachinery, Vol. 118, pp. 737–743.

2. Halstead DE, Wisler DC, Okiishi TH, Walker GJ, Hodson HP, Shin H-W (1995): Boundary layer development in axial compressors and turbines: Parts 1–4. ASME Papers 95-GT-461 to 95-GT-464.

3. Hodson HP, Gostelow JP (1999): Similarities in development between triggered turbulent spots and wake-induced turbulent patches. AIAA Paper 99–0404, 37th AIAA Aerospace Sciences Meeting, Reno, NV.

4. Schulte VS (1995): Unsteady separated boundary layers in axial-flow turbomachinery. PhD Thesis, Cambridge University.

5. Solomon WJ (1996): Unsteady boundary layer transition on axial compressor blades. PhD Thesis, University of Tasmania.

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