Estımatıon of hypersonıc unsteady and qausı-steady dampıng derıvatıves for a delta wings at large incıdence

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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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Bibliographic Details
Main Authors:	Renita, sharon Monis, Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	Science and Engineering Research Support Society 2020
Subjects:	TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) TL780 Rockets
Online Access:	http://irep.iium.edu.my/81244/ http://irep.iium.edu.my/81244/1/81244_Est%C4%B1mat%C4%B1on%20of%20Hyperson%C4%B1c%20Unsteady.pdf

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