Direct Numerical Simulation of a Supersonic Base Flow Behind a Circular Cylinder
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A supersonic flow in the near wake behind a cylinder is considered. Base pressure distributions behind a circular cylinder for various Mach numbers M∞ are obtained and analyzed by means of direct numerical simulation based on high-order approximation algorithms. For M∞ = 2.46, the results obtained in the present study are compared with available experimental and numerical data. Generation of turbulent kinetic energy is calculated for various Mach numbers.
Keywordssupersonic flow Navier–Stokes equations high-order approximation direct numerical simulation base drag
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- 1.A. V. Garbaruk, M. Kh. Strelets, and M. L. Shur, Modeling of Turbulence in Complex Flow Computations: Tutorial (Izd. Politekh. Univ., St. Petersburg, 2012) [in Russian].Google Scholar
- 6.D. R. Chapman, “An Analysis of Base Pressure at Supersonic Velocities and Comparison with Experiment,” Technical Note No. 2137 (Nat. Advisory Committee for Aeronautics, Washington, 1950).Google Scholar
- 10.R. D. Sandberg, “Stability Analysis of Axisymmetric Supersonic Wakes Using Various Basic States,” J. Phys.: Conf. Ser. 318, 032017 (2011).Google Scholar
- 14.A. M. Molchanov, Mathematical Modeling of Problems of Gas Dynamics and Heat and Mass Transfer (Moscow Aviation Institute, Moscow, 2013) [in Russian].Google Scholar