Numerical investigation of annular expansion-deflection nozzle flow under varying backpressure changing rate-Reference-Cited by-同舟云学术

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Numerical investigation of annular expansion-deflection nozzle flow under varying backpressure changing rate

Published:2024-08 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHOU Bocheng,WANG Ge,GUAN Ben,CHEN Yan,YANG Zenan

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference44 articles.

1. Advanced rocket nozzles;Hagemann;J Propuls Power,1998

2. Effect of two-phase flow on performance of plug nozzle in solid rocket motor;Li;Acta Aeronautica et Astronautica Sinica,2023

3. Goetz A, Hagemann G, Kretschmer J, et al. Advanced upper stage propulsion concept-The expansion-deflection upper stage. Reston: AIAA; 2005. Report No.: AIAA-2005-3752.

4. Mockenhaupt J, Felix G. Cold flow tests of forced deflection nozzles for integrated stage application. Reston: AIAA; 1981. Report No.: AIAA-1981-1420.

5. Analysis of a new concept rocket nozzle;Rao,1960

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