Abstract
A new algorithm has been developed for obtaining higher-order accuracy in upwind schemes for the Euler and Navier-Stokes equations. In this method, the compatibility relations for the Euler equations are used to construct formulas for the higher-order interpolates. By using these formulas, computed results are obtained for steady, inviscid flow through a nozzle and also steady, in viscid, and viscous flow over an airfoil. This approach provides an alternative to total-variation-diminishing and essentially nonoscillatory schemes.
Original language | English |
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Pages (from-to) | 251-256 |
Number of pages | 6 |
Journal | AIAA journal |
Volume | 31 |
Issue number | 2 |
DOIs | |
Publication status | Published - 1993 Feb |
Externally published | Yes |
ASJC Scopus subject areas
- Aerospace Engineering