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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Main Authors: Monis, Renita Sharon, Shabana, Ayesha, Crasta, Asha, Khan, Sher Afghan
Format: Article
Language:English
Published: International Organization of Scientific Research ( IOSR ) 2016
Subjects:
Online Access: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
id iium-54297
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spelling 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
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic QA Mathematics
QB Astronomy
spellingShingle 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
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