Abstract
Numerical simulations of a two-dimensional supersonic flow of an inviscid perfect gas over a double wedge in the Mach numbers range 5 ≤ M ≤ 9, revealed the existence of self-induced oscillations in the shock wave flow pattern in a narrow range of geometrical parameters.
Original language | English |
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Pages (from-to) | L85-L88 |
Journal | Physics of Fluids |
Volume | 15 |
Issue number | 12 |
DOIs | |
State | Published - 1 Jan 2003 |
ASJC Scopus subject areas
- Computational Mechanics
- Condensed Matter Physics
- Mechanics of Materials
- Mechanical Engineering
- Fluid Flow and Transfer Processes