Aerodynamic Shape Optimization of Doubly Offset Serpentine Diffuser using Response Surface Methodology-Reference-Cited by-同舟云学术

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Aerodynamic Shape Optimization of Doubly Offset Serpentine Diffuser using Response Surface Methodology

Published:2021-12-14 Issue: Volume: Page:
ISSN:
Container-title:2021 Seventh International Conference on Aerospace Science and Engineering (ICASE)
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Author:

Altaf Zohaib¹,Ali Arslan¹,Salamat Shuaib¹

Affiliation:

1. Air University,Aerospace & Aviation Campus,Aerospace Engineering Department,Kamra,Pakistan

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9904024/9904037/09904039.pdf?arnumber=9904039

Reference11 articles.

1. Subsonic diffuser design and performance for advanced fighter aircraft;l c c;Aircraft Design Systems and Operations Meeting,1985

2. Design optimization of a three-dimensional diffusing S-duct using a modified SST turbulent model;wenbiao;Aerospace Science and Technology,2016

3. Numerical Investigations of S-Shaped Air Inlet for Embedded Engines;leandro;Journal of Propulsion and Power,2019

4. Aircraft Propulsion;farokhi;Baseline Shape Optimized Shape,2014

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multi-objective shape optimization of doubly offset serpentine diffuser using Adjoint method;International Journal of Heat and Fluid Flow;2023-08

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