NUMERICAL SIMULATION OF TRANSONIC FLOW OVER SPACE VEHICLES
Natalia V. Palchekovskaya
Abstract
Natalia V. Palchekovskaya
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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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