Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number

Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number

This paper focusses attention on the influence of prominent curved ends to restraining deprived owing to the transverse frequency for the numerous amplitude, flow rebound perspective δ, hinge location, and the inertia. In the current learning by the consequence of expansion fan on the expansion side...

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Bibliographic Details
Main Authors: Renita, sharon Monis, Crasta, Asha, Khan, Sher Afghan
Format: Article
Language:English
English
Published: Testmagzine.biz 2020
Subjects:
TL500 Aeronautics
Online Access:http://irep.iium.edu.my/80194/
http://irep.iium.edu.my/80194/1/6133-Article%20Text-10869-1-10-20200420.pdf
http://irep.iium.edu.my/80194/7/80194%20-Analytical%20Estimation%20of%20Stability%20Derivatives_SCOPUS.pdf

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