DocumentCode :
8452
Title :
Desing and Analysis of an Unmanned Aerial Vehicle Propulsion System with Fluidic Flow Control Inside a Highly Compact Serpentine Inlet Duct
Author :
Charles E.Hall Jr استاد راهنما
University :
RaLeigh North caroLin astate university
Grade :
نامعلوم
Major :
Master of Science )Aerospace Engineering(
Number of pages :
0
Publish Date :
2003
Keyword :
UAV Propulsion System Distortion Turbojet
Note :
01
Language :
انگليسي
Link To Document :
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