Influences of the compressibility on aerodynamic characteristics of profile under the transonic flow theory
Transonic flows are complex problems. At certain Mach numbers, in gas flows there are local transitions from the subsonic into the supersonic and reciprocally, especially the discontinuity throughout shock waves. Subsonic flows and supersonic flows have very different properties, thus calculation me...
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| Format: | Article |
| Language: | English |
| Published: |
Publishing House for Science and Technology
2007-12-01
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| Series: | Vietnam Journal of Mechanics |
| Online Access: | https://vjs.ac.vn/index.php/vjmech/article/view/5598 |
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