Direct numerical simulation of flow past a sphere at a Reynolds number between 500 and 1000 in compressible flows-Reference-Cited by-同舟云学术

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Direct numerical simulation of flow past a sphere at a Reynolds number between 500 and 1000 in compressible flows

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Nagata Takayuki¹,Nonomura Taku¹,Takahashi Shun²,Mizuno Yusuke²,Fukuda Kota²

Affiliation:

1. Tohoku University

2. Tokai University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0381

Reference26 articles.

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2. Stability of the Low Reynolds Number Compressible Flow Past a NACA0012 Airfoil;AIAA Journal;2022-02

3. Particle-resolved simulations of shock-induced flow through particle clouds at different Reynolds numbers;Physical Review Fluids;2020-01-27

4. Experimental investigation of transonic and supersonic flow over a sphere for Reynolds numbers of 103–105 by free-flight tests with schlieren visualization;Shock Waves;2019-09-27

5. Schlieren visualization of transonic and supersonic flow over a sphere at Reynolds number between 103and 105through free-flight tests;AIAA Scitech 2019 Forum;2019-01-06

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