Flow distortion in a circular-to-rectangular transition duct
Author:
Affiliation:
1. National Cheng Kung University, Tainan, Taiwan, Republic of China
2. Chung-Shan Institute of Science and Technology, Taichung, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.25237
Reference21 articles.
1. Static Performance of Vectoring/Reversing Nonaxisymmetric Nozzles
2. Aerodynamic Effects Induced by a Vectored High Aspect Ratio Nonaxisymmetric Exhaust Nozzle
3. Performance Evaluation of an Air Vehicle Utilizing Nonaxisymrnetric Nozzles
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