RBF-POD reduced-order modeling of flow field in the curved shock compression inlet-Reference-Cited by-同舟云学术

RBF-POD reduced-order modeling of flow field in the curved shock compression inlet

Published:2021-08 Issue: Volume:185 Page:25-36
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Sun Fei,Su Wei-Yi,Wang Mou-Yuan,Wang Ren-Jie

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

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4. Dynamic characterization and active control of unstarts in a near-isentropic supersonic inlet, Master Dissertation, Aeronautics and Astronautics Dept;Ahsun;Massachusetts Inst. Technol.,2004

5. A method for generating reduced-order linear models of multidimensional supersonic inlets;Chicatelli;NASA/CR,1998

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