Numerical study of ways to prevent side loads in an over–expanded rocket nozzles during the launch stage-Reference-Cited by-同舟云学术

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Numerical study of ways to prevent side loads in an over–expanded rocket nozzles during the launch stage

Published:2019-10 Issue: Volume:163 Page:196-201
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ivanov I.E.,Kryukov I.A.

Funder

Russian academy of science

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. Two–dimensional over–expanded jet flow parameters in supersonic nozzle lip vicinity;Silnikov;Acta Astronaut.,2014

2. Incident shock strength evolution in overexpanded jet flow out of rocket nozzle;Silnikov;Acta Astronaut.,2017

3. European cooperation on flow separation control;Frey,2002

4. Side loads and thermal loads in rocket nozzles. overview CNES–ONERA ATAC programme;Reijasse;Int. J. Eng. Syst. Model Simul.,2011

5. Wall pressure unsteadiness and side loads in overexpanded rocket nozzles;Baars;AIAA J.,2012

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1. Experimental and numerical investigation on design parameters of slot nozzles;Aerospace Science and Technology;2023-10

2. 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

3. Numerical Study of Wall Heat Transfer Effects on Flow Separation in a Supersonic Overexpanded Nozzle;Energies;2023-02-10

4. Numerical Study of Viscous Flows in Rocket Engine Nozzles with an Optimized Supersonic Part and Separation of the Laminar Boundary Layer from the Wall;Russian Aeronautics;2022-10

5. Numerical study of the separation of a turbulent boundary in rocket engine nozzles with an optimized supersonic part;Journal of Physics: Conference Series;2022-07-01

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