DocumentCode :
13346
Title :
Two-Dimensional Shock Sensitivity Analysis for Transonic Airfoils with Leading-edge and Trailing-edge Device Deflections
Author :
William H. Mason استاد راهنما , B. Grossman استاد مشاور , J. A. Schetz استاد مشاور
University :
Virginia Polytechnic Institute and state University
Grade :
نامعلوم
Major :
Master of Engineering )Aerospace and Ocean Engineering(
Number of pages :
0
Publish Date :
2001
Keyword :
2-D flow separation , device deflection , shock movement , transonic airfoil
Note :
01
Language :
انگليسي
Link To Document :
بازگشت