Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge
Accurate estimation of the aerodynamic stability derivatives of airplanes is essential to evaluate the performance of the aircraft, whether civilian or military. Theoretical prediction methods for the dynamic stability derivatives at high angles of attack have not advanced, and in the present paper...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Transstellar Journal Publications and Research Consultancy Private Limited (TJPRC)
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/75483/ http://irep.iium.edu.my/75483/ http://irep.iium.edu.my/75483/ http://irep.iium.edu.my/75483/1/2-67-1571463142-IJMPERDOCT201922.pdf http://irep.iium.edu.my/75483/7/75483_Estimation%20of%20damping%20derivatives_scopus.pdf |