Effect of angle of incidence on stability derivatives of a wing

In the Present paper effect of angle of incidence on pitching derivatives of a delta wing with curved leading edges of a attached shock case is been studied. A Strip theory is used in which strips at different span wise location are independent. This combines with similitude to give a piston theory....

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Main Authors:	Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	http://www.ijraset.com/fileserve.php?FID=491 2014
Subjects:	TL787 Astronautics
Online Access:	http://irep.iium.edu.my/49938/ http://irep.iium.edu.my/49938/ http://irep.iium.edu.my/49938/1/49938.pdf

id	iium-49938
recordtype	eprints
spelling	iium-499382018-06-12T03:39:08Z http://irep.iium.edu.my/49938/ Effect of angle of incidence on stability derivatives of a wing Crasta, Asha Khan, Sher Afghan TL787 Astronautics In the Present paper effect of angle of incidence on pitching derivatives of a delta wing with curved leading edges of a attached shock case is been studied. A Strip theory is used in which strips at different span wise location are independent. This combines with similitude to give a piston theory. From the results it is found that stiffness and damping derivatives in pitch increasing linearly up to angle of attack 250 and then non-linearity creeps in. The Present theory is valid only for attached shock case. Effects of wave reflection and viscosity have not been taken into account. Results have been obtained for hypersonic flow of perfect gases over a wide range of angle of attack and Mach number. http://www.ijraset.com/fileserve.php?FID=491 2014-05 Article PeerReviewed application/pdf en http://irep.iium.edu.my/49938/1/49938.pdf Crasta, Asha and Khan, Sher Afghan (2014) Effect of angle of incidence on stability derivatives of a wing. International Journal for Research in Applied Science and Engineering Technology (IJRASET), 2 (V). pp. 411-422. ISSN 2321-9653 http://www.ijraset.com/fileserve.php?FID=491
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TL787 Astronautics
spellingShingle	TL787 Astronautics Crasta, Asha Khan, Sher Afghan Effect of angle of incidence on stability derivatives of a wing
description	In the Present paper effect of angle of incidence on pitching derivatives of a delta wing with curved leading edges of a attached shock case is been studied. A Strip theory is used in which strips at different span wise location are independent. This combines with similitude to give a piston theory. From the results it is found that stiffness and damping derivatives in pitch increasing linearly up to angle of attack 250 and then non-linearity creeps in. The Present theory is valid only for attached shock case. Effects of wave reflection and viscosity have not been taken into account. Results have been obtained for hypersonic flow of perfect gases over a wide range of angle of attack and Mach number.
format	Article
author	Crasta, Asha Khan, Sher Afghan
author_facet	Crasta, Asha Khan, Sher Afghan
author_sort	Crasta, Asha
title	Effect of angle of incidence on stability derivatives of a wing
title_short	Effect of angle of incidence on stability derivatives of a wing
title_full	Effect of angle of incidence on stability derivatives of a wing
title_fullStr	Effect of angle of incidence on stability derivatives of a wing
title_full_unstemmed	Effect of angle of incidence on stability derivatives of a wing
title_sort	effect of angle of incidence on stability derivatives of a wing
publisher	http://www.ijraset.com/fileserve.php?FID=491
publishDate	2014
url	http://irep.iium.edu.my/49938/ http://irep.iium.edu.my/49938/ http://irep.iium.edu.my/49938/1/49938.pdf
first_indexed	2023-09-18T21:10:34Z
last_indexed	2023-09-18T21:10:34Z
_version_	1777411224589303808

Effect of angle of incidence on stability derivatives of a wing

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