DocumentCode :
8776
Title :
The Influence of Pressure Ratio on Film Cooling Performance of a Turbine Blade
Author :
Wing Ng استاد مشاور , Joseph Schetz استاد مشاور , Thomas Diller استاد راهنما
University :
Virginia Polytechnic Institute and state University
Grade :
نامعلوم
Major :
Master of Science )Mechanical Engineering(
Number of pages :
0
Publish Date :
1999
Keyword :
Turbine , Film cooling , heat transfer , Transonic cascade
Note :
01
Language :
انگليسي
Link To Document :
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