Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow

In this paper unified supersonic theory is used to derive the expressions of Stiffness derivative of a wedge in Hypersonic flow. This paper demonstrates the effects of pivot position on the stffness derivative with Mach number and incidence angle. From the above discussion it is seen that behaviour...

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Main Authors:	Crasta, Asha, Shabana, Aysha, Monis, Renita, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	International Organization of Scientific Research ( IOSR ) 2016
Subjects:	V Naval Science (General)
Online Access:	http://irep.iium.edu.my/54287/ http://irep.iium.edu.my/54287/ http://irep.iium.edu.my/54287/1/Asha.pdf

id	iium-54287
recordtype	eprints
spelling	iium-542872017-01-31T06:18:45Z http://irep.iium.edu.my/54287/ Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow Crasta, Asha Shabana, Aysha Monis, Renita Khan, Sher Afghan V Naval Science (General) In this paper unified supersonic theory is used to derive the expressions of Stiffness derivative of a wedge in Hypersonic flow. This paper demonstrates the effects of pivot position on the stffness derivative with Mach number and incidence angle. From the above discussion it is seen that behaviour of the stiffness derivative is the same for h = 0 to 0.4 and also for h = 0.8, 0.9, and 1.0. Due to the pivot position variations there is a significant variation of Stiffness derivative with Mach number and incidence angle. International Organization of Scientific Research ( IOSR ) 2016-12 Article PeerReviewed application/pdf en http://irep.iium.edu.my/54287/1/Asha.pdf Crasta, Asha and Shabana, Aysha and Monis, Renita and Khan, Sher Afghan (2016) Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow. IOSR Journal of Mechanical & Civil Engineering, 12 (6). pp. 97-104. ISSN 2320-334x E-ISSN 2278-1684 http://www.iosrjournals.org/iosr-jmce/pages/i-%20CAM2K16(Mech)-volume-3.html
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	V Naval Science (General)
spellingShingle	V Naval Science (General) Crasta, Asha Shabana, Aysha Monis, Renita Khan, Sher Afghan Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
description	In this paper unified supersonic theory is used to derive the expressions of Stiffness derivative of a wedge in Hypersonic flow. This paper demonstrates the effects of pivot position on the stffness derivative with Mach number and incidence angle. From the above discussion it is seen that behaviour of the stiffness derivative is the same for h = 0 to 0.4 and also for h = 0.8, 0.9, and 1.0. Due to the pivot position variations there is a significant variation of Stiffness derivative with Mach number and incidence angle.
format	Article
author	Crasta, Asha Shabana, Aysha Monis, Renita Khan, Sher Afghan
author_facet	Crasta, Asha Shabana, Aysha Monis, Renita Khan, Sher Afghan
author_sort	Crasta, Asha
title	Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
title_short	Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
title_full	Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
title_fullStr	Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
title_full_unstemmed	Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
title_sort	analysis of variation of stiffness derivative with mach number and angle of attack for a supersonic flow
publisher	International Organization of Scientific Research ( IOSR )
publishDate	2016
url	http://irep.iium.edu.my/54287/ http://irep.iium.edu.my/54287/ http://irep.iium.edu.my/54287/1/Asha.pdf
first_indexed	2023-09-18T21:16:49Z
last_indexed	2023-09-18T21:16:49Z
_version_	1777411617525334016

Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow

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