Effect of sweptback angle of a delta wing on surface pressure distribution at supersonic Mach numbers
This work aims to shed light on the effect of the pivot position on the surface pressure distribution over a 3D wing in different flight conditions. The study is intended to support the design and development of aerospace vehicles where stability analysis, performance optimization, and aircraft desi...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | en |
| Published: |
Tech Science Press
2024
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/114665/7/114665_Effect%20of%20Sweptback%20Angle%20of%20a%20Delta%20Wing%20on%20Surface%20Pressure%20Distribution%20at%20Supersonic%20Mach%20Numbers.pdf http://irep.iium.edu.my/114665/ https://www.techscience.com/fdmp/v20n10/58028 |
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