Computation of subsonic inviscid flow past a cone using high-order schemes
A wake-dominated unsteady flow of Mach number 0.2 past a cone of vertex angle 60 deg is calculated numerically using high-order finite difference schemes on structured grids. The three-dimensional compressible Euler equations are solved to simulated an inviscid flow that exhibits large fluctuations...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
2002-10-01.
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| Subjects: | |
| Online Access: | Get fulltext |