Computation of stability derivative for a wing for specific heat ratio= 1.66 for hypersonic flow
The flight performance of aircraft relies on aerodynamic non-dimensional parameters like the drag coefficient, lift coefficient, and the moment coefficient of the aerospace vehicles. The knowledge of these properties is supremely necessary for optimal design, and thus the aerodynamics and the perfo...
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| Main Authors: | , , , |
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| 格式: | Article |
| 語言: | English |
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TJPRC Pvt. Ltd
2020
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| 在線閱讀: | http://irep.iium.edu.my/80867/1/22splissuejun2020ijmperd22j.pdf http://irep.iium.edu.my/80867/ http://www.tjprc.org/journals/journal-of-mechanical-engineering |
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