Direct numerical simulation of flow around a heated/cooled isolated sphere up to a Reynolds number of 300 under subsonic to supersonic conditions

Author:

Nagata TakayukiORCID,Nonomura Taku,Takahashi Shun,Mizuno Yusuke,Fukuda Kota

Funder

JSPS KAKENHI

Tokai University

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference34 articles.

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2. T. Ishii, S. Tsutsumi, K. Ui, S. Tokudome, Y. Ishii, K. Wada, S. Nakamura, Acoustic measurement of 1:42 scale booster and launch pad, in: Proceedings of Meetings on Acoustics, vol. 18, no. 1, 2014, pp. 040009.

3. S. Tsutsumi, T. Shimizu, R. Takaki, E. Shima, M. Arita, K. Fujii, Numerical study of pressure waves generated by H-IIA launch vehicle at lift-off, in: Conference Proceedings of AJCPP 2008, Gyeongju, Korea, 6–8 March 2008, pp. 266–271.

4. Study on acoustic prediction and reduction of epsilon launch vehicle at liftoff;Tsutsumi;J. Spacecraft Rockets,2014

5. Computational prediction of acoustic waves from a subscale rocket motor;Nonomura;Trans. JSASS Aerospace Thec. Jpn.,2014

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