An effect of sweep angle on roll damping derivative for a Delta wing with curved leading edges in unsteady flow
This paper presents the results of an analytical study to account the effect of the sweep angle of a delta wing whose leading edges are curved on roll damping derivative at various angles of attack and the amplitude of the full sine waves. In the present theory, the effect of Leeward surface has b...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Transstellar Journal Publications and Research
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/70995/ http://irep.iium.edu.my/70995/ http://irep.iium.edu.my/70995/ http://irep.iium.edu.my/70995/1/70995_An%20effect%20of%20sweep%20angle%20on%20roll%20damping.pdf http://irep.iium.edu.my/70995/2/70995_An%20effect%20of%20sweep%20angle%20on%20roll%20damping_Scopus.pdf |
Internet
http://irep.iium.edu.my/70995/http://irep.iium.edu.my/70995/
http://irep.iium.edu.my/70995/
http://irep.iium.edu.my/70995/1/70995_An%20effect%20of%20sweep%20angle%20on%20roll%20damping.pdf
http://irep.iium.edu.my/70995/2/70995_An%20effect%20of%20sweep%20angle%20on%20roll%20damping_Scopus.pdf