DocumentCode
11967
Title
Noise Reduction in an Axisymmetric Supersonic Aircraft Inlet using Trailing Edge Blowing
Author
Wing Ng استاد راهنما , C. L. Dancey استاد مشاور , J. L. Fleming استاد مشاور , Ricardo D. Burdisso استاد مشاور
University
Virginia Polytechnic Institute and state University
Grade
نامعلوم
Major
Master of Science )Mechanical Engineering(
Number of pages
0
Publish Date
1998
Keyword
Turbomachinery , Noise , aeroacoustics , STRUTS
Note
01
Language
انگليسي
Link To Document