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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/54287/1/Asha.pdf
http://irep.iium.edu.my/54287/
http://www.iosrjournals.org/iosr-jmce/pages/i-%20CAM2K16(Mech)-volume-3.html
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spelling my.iium.irep.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 REM 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 http://www.iosrjournals.org/iosr-jmce/pages/i-%20CAM2K16(Mech)-volume-3.html
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
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/54287/1/Asha.pdf
http://irep.iium.edu.my/54287/
http://www.iosrjournals.org/iosr-jmce/pages/i-%20CAM2K16(Mech)-volume-3.html
_version_ 1643614522185875456
score 13.211869

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