Numerical investigation of surface roughness effects on non-equilibrium flow in expansion section of rocket nozzle-Reference-Cited by-同舟云学术

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Numerical investigation of surface roughness effects on non-equilibrium flow in expansion section of rocket nozzle

Published:2022-05 Issue: Volume:124 Page:107523
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Liu Yang^ORCID,Wang Hai-feng,Ma Dong,Gao Yong-gang,Zhao Wei

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. Direct numerical simulation of fine flow structures of subsonic-supersonic mixing layer;Liu;Aerosp. Sci. Technol.,2019

2. Direct numerical simulation of subsonic–supersonic mixing layer;Zhang;Acta Astronaut.,2018

3. Transition in open flow systems-a reassessment;Morkovin;Bull. Am. Phys. Soc.,1994

4. Turbulence statistics and structures of a supersonic boundary layer by direct numerical simulation;Liu;Phys. Gases,2021

5. Hypersnonic boundary layer transition: what we know, where shall we go;Chen;Acta Aerodyn. Sin.,2017

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1. ZrO2-reinforced polymer-matrix composites used for thermal protection systems of ultra-high temperature aerospace propulsion;Aerospace Science and Technology;2024-02

2. Study on the Influence of Nozzle Ablation on the Performance of the Solid Rocket Motor;Aerospace;2023-02-09

3. Self-assembled archaea bio-coatings in thermal-fluids systems: A study on adhesion optimization and energy efficiency;International Journal of Thermofluids;2022-08

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