Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow
n the present paper a theory for 2D slender bodies at high angle of attack in hypersonic flow has been developed to determine the aerodynamic derivatives in pitch for different Mach numbers. The present theory has been applied to a sharp thick wedge with attached shock case. Using the theory, a rela...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Indian Society for Education and Environment & Informatics Publishing Limited
2016
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/53877/ http://irep.iium.edu.my/53877/ http://irep.iium.edu.my/53877/ http://irep.iium.edu.my/53877/1/SAKHAN.pdf |