Direct numerical simulation of Mach-s wave propagation in su-personic flow
- 1 Corresponding Member of RAS, Dr.Sc. (Phys.-Math.), Professor, Lecturer, Moscow Physical Technical Institute; Head of Department, Central Aero-hydrodynamic Institute named after N.E. Zhukovsky
- 2 Ph.D. (Phys.-Math.), Associate Professor, Lecturer, Moscow Physical Technical Institute
- 3 Post-graduate Student, Moscow Physical Technical Institute
Abstract
The paper presents the method direct numerical simulation of disturbance Mach-s wave in supersonic flow. The simulation results of mass flow and pulsation levels of mass flow are presented. Results of numerical simulation of mass flow and pulsation are compared with the experimental results at Mach number M = 2.5, Reynolds number Re = 5*106 and stagnation temperature T = 293 K. We used second - order approximation in time and third - order approximation in space.
How to cite
Егоров И.В., Федоров А.В., Хоанг Д.К. Метод прямого численного моделирования распространения волны Маха в сверхзвуковом потоке // Электромагнитные волны и электронные системы. 2015. № 5. С. 22–27.
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