Analysis of the Magnus Moment Aerodynamic Characteristics of Rotating Missiles at High Altitudes
The Magnus moment characteristics of rotating missiles with Mach numbers of 1.3 and 1.5 at different altitudes and angles of attack were numerically simulated based on the transition SST model. It was found that the Magnus moment direction of the missiles changed with the increase of the angle of at...
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| Hlavní autoři: | , , |
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| Médium: | Artigo |
| Jazyk: | Inglês |
| Vydáno: |
Wiley
2021-01-01
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| Edice: | International Journal of Aerospace Engineering |
| On-line přístup: | http://dx.doi.org/10.1155/2021/6623510 |
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