A generative adversarial network for enhancing over-expansion flow field perception of nozzles with large expansion ratio-Reference-Cited by-同舟云学术

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A generative adversarial network for enhancing over-expansion flow field perception of nozzles with large expansion ratio

Published:2024-08 Issue: Volume:151 Page:109324
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Yunfei^ORCID,Guo Wanlin^ORCID

Publisher

Elsevier BV

Reference58 articles.

1. Modelling side loads in separated rocket nozzles;Aghababaie,2011

2. Characteristics of space shuttle main engine failures;Cikanek,1987

3. Le-7a engine nozzle problems during transient operations;Watanabe,2002

4. Redesign of the vulcain 2 nozzle extension;Winterfeldt,2005

5. Experimental study of gas-flow separation in overexpanded exhaust nozzles for rocket motors;Cowles,1949

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