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