Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number
This paper focusses attention on the influence of prominent curved ends to restraining deprived owing to the transverse frequency for the numerous amplitude, flow rebound perspective δ, hinge location, and the inertia. In the current learning by the consequence of expansion fan on the expansion side...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Testmagzine.biz
2020
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/80194/ http://irep.iium.edu.my/80194/1/6133-Article%20Text-10869-1-10-20200420.pdf http://irep.iium.edu.my/80194/7/80194%20-Analytical%20Estimation%20of%20Stability%20Derivatives_SCOPUS.pdf |