Aerodynamic Parameters Analysis of Transonic Flow Past Unswept and Swept Wings
The transonic flow past unswept and swept wings has been studied. For this purpose the transonic potential flow equation is solved for inviscid compressible flow. The shock waves are replaced by discontinuities across which the entropy is conserved. The velocity field and pressure coefficients are e...
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| Format: | Article |
| Language: | English |
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Unviversity of Technology- Iraq
2011-03-01
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| Series: | Engineering and Technology Journal |
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| Online Access: | https://etj.uotechnology.edu.iq/article_30763_aa766e183f724f2aba96308e2d1e7d46.pdf |