Estımatıon of hypersonıc unsteady and qausı-steady dampıng derıvatıves for a delta wings at large incıdence
This paper presents results of quasi-steady and unsteady damping derivatives of a delta wing whose leading edge is straight. Results are computed for a wide range of Mach numbers and angles of attack. Here the contribution to the damping derivatives due to the rate of change of angle of attack is es...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Science and Engineering Research Support Society
2020
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/81244/1/81244_Est%C4%B1mat%C4%B1on%20of%20Hyperson%C4%B1c%20Unsteady.pdf http://irep.iium.edu.my/81244/ http://sersc.org/journals/index.php/ijast |
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