Nozzle design optimization for supersonic wind tunnel by using surrogate-assisted evolutionary algorithms-Reference-Cited by-同舟云学术

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Nozzle design optimization for supersonic wind tunnel by using surrogate-assisted evolutionary algorithms

Published:2022-11 Issue: Volume:130 Page:107879
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Matsunaga Masanobu^ORCID,Fujio Chihiro^ORCID,Ogawa Hideaki^ORCID,Higa Yoshitaka,Handa Taro^ORCID

Funder

Tohoku University Institute of Fluid Science

Japan Society for the Promotion of Science

International Foundation for Science

Tohoku University

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. Low-frequency unsteadiness of shock-wave/boundary-layer interaction in an isolator with background waves;Wang;Phys. Fluids,2020

2. Verification and validation of CFD simulations;Stern,1999

3. Wind tunnel testing's future: generation of wind tunnel test requirements and facilities;Melanson,2010

4. Fundamentals of wind-tunnel design;Cattafesta;Encycl. Aerosp. Eng.,2010

5. Modern Compressible Flow with Historical Perspective;Anderson,2020

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4. A shape design optimization methodology based on the method of characteristics for rocket nozzles;CEAS Space Journal;2023-07-08

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