Journal of Applied Mathematics and Physics

Vol.2 No.6(2014), Paper ID 46034, 6 pages

DOI:10.4236/jamp.2014.26054

 

Aerodynamic Optimization of the Expansion Section in a Hypersonic Quiet Nozzle Based on Favorable Pressure Effect

 

Jian Gong, Dapeng Yao, Xunhua Liu

 

China Academy of Aerospace Aerodynamics, Beijing, 100074, China
China Academy of Aerospace Aerodynamics, Beijing, 100074, China
China Academy of Aerospace Aerodynamics, Beijing, 100074, China

 

Copyright © 2014 Jian Gong, Dapeng Yao, Xunhua Liu et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

 

How to Cite this Article


Gong, J. , Yao, D. and Liu, X. (2014) Aerodynamic Optimization of the Expansion Section in a Hypersonic Quiet Nozzle Based on Favorable Pressure Effect. Journal of Applied Mathematics and Physics, 2, 443-448. doi: 10.4236/jamp.2014.26054.

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