This paper, as Part II of the study on wake-disturbed boundary layer, is aimed at investigation of the effects of free-stream turbulence on wake-induced transition of the boundary layer under a favorable pressure gradient. Hot-wire probe measurements are also made on the wake-disturbed boundary layer to obtain ensemble-averaged shape factor contours on the distance-time diagrams. These data are then used to examine how the favorable pressure gradient and the free-stream turbulence affects time-resolved behaviors of the boundary layer subjected to periodic wakes. In addition, likewise in Part I, the heat transfer data are compared with the transition model proposed by Funazaki (1996) in order to check the capability of the model under the favorable pressure gradient as well as the free-stream turbulence.
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ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7868-2
PROCEEDINGS PAPER
Studies on Wake-Disturbed Boundary Layers Under the Influences of Favorable Pressure Gradient and Free-Stream Turbulence: Part II — Effect of Free-Stream Turbulence
Ken-ichi Funazaki,
Ken-ichi Funazaki
Iwate University, Morioka, Japan
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Takashi Kitazawa,
Takashi Kitazawa
Iwate University, Morioka, Japan
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Kazuyuki Koizumi,
Kazuyuki Koizumi
Iwate University, Morioka, Japan
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Tadashi Tanuma
Tadashi Tanuma
Toshiba Corporation, Yokohama, Japan
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Ken-ichi Funazaki
Iwate University, Morioka, Japan
Takashi Kitazawa
Iwate University, Morioka, Japan
Kazuyuki Koizumi
Iwate University, Morioka, Japan
Tadashi Tanuma
Toshiba Corporation, Yokohama, Japan
Paper No:
97-GT-452, V001T03A078; 9 pages
Published Online:
December 24, 2014
Citation
Funazaki, K, Kitazawa, T, Koizumi, K, & Tanuma, T. "Studies on Wake-Disturbed Boundary Layers Under the Influences of Favorable Pressure Gradient and Free-Stream Turbulence: Part II — Effect of Free-Stream Turbulence." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. Orlando, Florida, USA. June 2–5, 1997. V001T03A078. ASME. https://doi.org/10.1115/97-GT-452
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