Design of Optimal Conical Camber for Minimum Induced Drag of a Delta Wing |
Author(s): |
| Satish Chander Gupta , MVJ College of Engineering |
Keywords: |
| Optimal Conical Camber, Delta Wing |
Abstract |
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Minimising of the drag due to lift in supersonic flow is attempted herein. A flat surface wing is optimized for minimum induced drag for a supersonic Mach number. Optimal warp is separated into twist and camber. Wing for fighter aircraft role is considered. Supersonic optimal warp is also compared with that resulting from a subsonic Mach number. |
Other Details |
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Paper ID: IJSRDV13I20095 Published in: Volume : 13, Issue : 2 Publication Date: 01/05/2025 Page(s): 206-210 |
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