2020•International Journal of Fluid Mechanics ResearchRequires access

NUMERICAL SIMULATION OF TRANSONIC FLOW OVER SPACE VEHICLES

Natalia V. Palchekovskaya

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Abstract

In this study peculiarities of transonic flow over a space vehicle similar to that of the ExoMars project are studied numerically. Dependencies of axial force coefficients on Mach number are obtained. Flow field transformation is shown when Mach number changes from subsonic to supersonic values. Critical Mach number, at which local supersonic zones disappear, is found.

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What this paper is about

In this study peculiarities of transonic flow over a space vehicle similar to that of the ExoMars project are studied numerically. Dependencies of axial force coefficients on Mach number are obtained. Flow field transformation is shown when Mach number changes from subsonic to supersonic values. Critical Mach number, at which local supersonic zones disappear, is found.

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Available abstract

In this study peculiarities of transonic flow over a space vehicle similar to that of the ExoMars project are studied numerically. Dependencies of axial force coefficients on Mach number are obtained. Flow field transformation is shown when Mach number changes from subsonic to supersonic values. Critical Mach number, at which local supersonic zones disappear, is found.

Key concepts: Transonic, Mach number, Supersonic speed, Mechanics, Drag divergence Mach number, Choked flow, Aerospace engineering, Physics

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