Computational investigation of flow separation in a thrust-optimized parabolic nozzle during high-altitude testing-Reference-Cited by-同舟云学术

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Computational investigation of flow separation in a thrust-optimized parabolic nozzle during high-altitude testing

Published:2020-01 Issue: Volume:197 Page:104363
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Lee Changsoo,Choi Kyungjun,Kim Chongam^ORCID,Han Sanghoon

Funder

Korea Institute of Science and Technology Information

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference33 articles.

1. Sea level side loads in high-area-ratio rocket engines;Nave,1973

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

3. LE-7A engine nozzle problems during the transient operations;Watanabe,2002

4. Redesign of the Vulcain 2 Nozzle Extension;Winterfeldt,2005

5. Shock pattern in the plume of rocket nozzles: needs for design consideration;Hagemann;Shock Waves,2008

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1. Flow Effects and Propulsion Performance on Various Single Expansion Ramp Nozzle Configurations of Scramjet Engine;Symmetry;2024-08-14

2. Numerical analysis of jet noise for nozzles with different throat sizes;AIP Advances;2024-06-01

3. The Influence of External Flow Field on the Flow Separation of Overexpanded Single-Expansion Ramp Nozzle;Aerospace;2023-11-13

4. Design and analysis of a supersonic diffuser for altitude testing of upper-stage liquid rocket engines;Aerospace Science and Technology;2023-11

5. Experimental and comprehensive investigation of second throat diffuser area effect on ground test of a thrust optimized parabolic nozzle with different expansion ratios;Acta Astronautica;2023-08

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