Effect of sweep angle and a half sine wave on roll damping derivative of a Delta Wing
This paper presents the effect of sweep angle on a roll of damping derivative of a delta wing with half-sine wave for an attached shock case in supersonic/hypersonic flow has been studied analytically. The Ghosh Strip theory is replicated. By combining this with the similitude at high-speed flows l...
محفوظ في:
| المؤلفون الرئيسيون: | , , , |
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| التنسيق: | مقال |
| اللغة: | English English |
| منشور في: |
Blue Eyes Intelligence Engineering & Sciences
2019
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| الموضوعات: | |
| الوصول للمادة أونلاين: | http://irep.iium.edu.my/73973/1/Asha.pdf http://irep.iium.edu.my/73973/7/73973_Effect%20of%20sweep%20angle%20and%20a%20half%20sine%20wave%20on%20roll%20damping%20derivative%20of%20a%20delta%20wing_Scopus.pdf http://irep.iium.edu.my/73973/ https://www.ijrte.org/wp-content/uploads/papers/v8i2S3/B11840782S319.pdf |
| الوسوم: |
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الانترنت
http://irep.iium.edu.my/73973/1/Asha.pdfhttp://irep.iium.edu.my/73973/7/73973_Effect%20of%20sweep%20angle%20and%20a%20half%20sine%20wave%20on%20roll%20damping%20derivative%20of%20a%20delta%20wing_Scopus.pdf
http://irep.iium.edu.my/73973/
https://www.ijrte.org/wp-content/uploads/papers/v8i2S3/B11840782S319.pdf