Ensuring safe descend of reusable rocket stages – Numerical simulation and experiments on subsonic turbulent air flow around a semi-circular cylinder at zero angle of attack and moderate Reynolds number-Reference-Cited by-同舟云学术

Ensuring safe descend of reusable rocket stages – Numerical simulation and experiments on subsonic turbulent air flow around a semi-circular cylinder at zero angle of attack and moderate Reynolds number

Published:2018-09 Issue: Volume:150 Page:117-136
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Isaev Sergey,Baranov Paul,Popov Igor,Sudakov Alexander,Usachov Alexander,Guvernyuk Sergey,Sinyavin Alexei,Chylunin Alexei,Mazo Alexander,Kalinin Eugeny

Funder

Government of the Russian Federation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

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4. Controlling the turbulent flow past a thick airfoil by means of flow enhancement in a vortex cells using suction from central body surfaces;Baranov;Fluid Dyn.,2003

5. Modeling the increase in aerodynamic efficiency for a thick (37.5% chord) airfoil with slot suction in vortex cells with allowance for the compressibility effect;Isaev;Tech. Phys. Lett.,2015

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