Research output: Contribution to journal › Article › peer-review
The results of the numerical investigation of supersonic flow past a sharp slender body at an angle of attack are given with reference to the example of an axisymmetric cylindrical body with a conical nose. Separated and vortex structures developed at various angles of attack are identified. The effect of anomalous increase in pressure on the leeward side is explained.
Original language | English |
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Pages (from-to) | 653-656 |
Number of pages | 4 |
Journal | Fluid Dynamics |
Volume | 55 |
Issue number | 5 |
DOIs | |
State | Published - 1 Sep 2020 |
ID: 70201666