Supersonic flow analysis and evaluation of damping derivative
The emphasis of this paper is to examine the variation of damping derivative with incidence angle and Mach number with varying pivot position. The damping derivative decreases with Mach number and increases with the incidence angle. It is also seen that for a given Mach number the damping derivative...
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International Organization of Scientific Research ( IOSR )
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iium-542972017-01-25T02:46:03Z http://irep.iium.edu.my/54297/ Supersonic flow analysis and evaluation of damping derivative Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan QA Mathematics QB Astronomy The emphasis of this paper is to examine the variation of damping derivative with incidence angle and Mach number with varying pivot position. The damping derivative decreases with Mach number and increases with the incidence angle. It is also seen that for a given Mach number the damping derivatives are decreasing and reaches a minimum value and then again increases and attains the same value which was at h = 0, for pivot position h = 0 to h = 1.0 and at h = 0.5 it attains a minimum value and then increases for h = 0.6 to h = 1. The Damping derivative decreases with Mach number for the varying pivot position. International Organization of Scientific Research ( IOSR ) 2016-12 Article PeerReviewed application/pdf en http://irep.iium.edu.my/54297/1/Renita.pdf Monis, Renita Sharon and Shabana, Ayesha and Crasta, Asha and Khan, Sher Afghan (2016) Supersonic flow analysis and evaluation of damping derivative. IOSR Journal of Mechanical & Civil Engineering (IOSR-JMCE), 18 (6). pp. 29-36. ISSN 2320-334x E-ISSN 2278-1684 http://www.iosrjournals.org/iosr-jmce/papers/i-%20CAM2K16-2016/Mech/Volume%203/5.%2029-36.pdf 10.9790/1684-16053032936 |
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QA Mathematics QB Astronomy |
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QA Mathematics QB Astronomy Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan Supersonic flow analysis and evaluation of damping derivative |
description |
The emphasis of this paper is to examine the variation of damping derivative with incidence angle and Mach number with varying pivot position. The damping derivative decreases with Mach number and increases with the incidence angle. It is also seen that for a given Mach number the damping derivatives are decreasing and reaches a minimum value and then again increases and attains the same value which was at h = 0, for pivot position h = 0 to h = 1.0 and at h = 0.5 it attains a minimum value and then increases for h = 0.6 to h = 1. The Damping derivative decreases with Mach number for the varying pivot position. |
format |
Article |
author |
Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan |
author_facet |
Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan |
author_sort |
Monis, Renita Sharon |
title |
Supersonic flow analysis and evaluation of damping derivative |
title_short |
Supersonic flow analysis and evaluation of damping derivative |
title_full |
Supersonic flow analysis and evaluation of damping derivative |
title_fullStr |
Supersonic flow analysis and evaluation of damping derivative |
title_full_unstemmed |
Supersonic flow analysis and evaluation of damping derivative |
title_sort |
supersonic flow analysis and evaluation of damping derivative |
publisher |
International Organization of Scientific Research ( IOSR ) |
publishDate |
2016 |
url |
http://irep.iium.edu.my/54297/ http://irep.iium.edu.my/54297/ http://irep.iium.edu.my/54297/ http://irep.iium.edu.my/54297/1/Renita.pdf |
first_indexed |
2023-09-18T21:16:50Z |
last_indexed |
2023-09-18T21:16:50Z |
_version_ |
1777411619001729024 |