Computation of stiffness derivative for an unsteady delta wing with curved leading edges

An attempt has been made to derive the expressions for stiffness derivative for a delta wing with curved leading edges for an unsteady high speed flow. It is evident from the figures that stiffness derivative decreases as Mach number increases. It is also seen that as amplitude of half sine wave i...

Full description

Bibliographic Details
Main Authors:	Monis, Renita Sharon, Shabana, Ayesha, Crasta, Asha, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	Institute of Institutional Industrial Research 2017
Subjects:	QA297 Numerical Analysis
Online Access:	http://irep.iium.edu.my/61843/ http://irep.iium.edu.my/61843/ http://irep.iium.edu.my/61843/1/Paper-5-IJRRA-04-04-18.pdf

id	iium-61843
recordtype	eprints
spelling	iium-618432018-02-05T07:43:41Z http://irep.iium.edu.my/61843/ Computation of stiffness derivative for an unsteady delta wing with curved leading edges Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan QA297 Numerical Analysis An attempt has been made to derive the expressions for stiffness derivative for a delta wing with curved leading edges for an unsteady high speed flow. It is evident from the figures that stiffness derivative decreases as Mach number increases. It is also seen that as amplitude of half sine wave increases the stiffness derivative also increases. This is an improvement of previous theory as the effect of leeward surface are included in the present work. Institute of Institutional Industrial Research 2017-12 Article PeerReviewed application/pdf en http://irep.iium.edu.my/61843/1/Paper-5-IJRRA-04-04-18.pdf Monis, Renita Sharon and Shabana, Ayesha and Crasta, Asha and Khan, Sher Afghan (2017) Computation of stiffness derivative for an unsteady delta wing with curved leading edges. International Journal of Recent Research Aspects .., 4 (4). pp. 69-72. ISSN 2349-7688 https://www.ijrra.net/Vol4issue4/IJRRA-04-04-18.pdf
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	QA297 Numerical Analysis
spellingShingle	QA297 Numerical Analysis Monis, Renita Sharon Shabana, Ayesha Crasta, Asha Khan, Sher Afghan Computation of stiffness derivative for an unsteady delta wing with curved leading edges
description	An attempt has been made to derive the expressions for stiffness derivative for a delta wing with curved leading edges for an unsteady high speed flow. It is evident from the figures that stiffness derivative decreases as Mach number increases. It is also seen that as amplitude of half sine wave increases the stiffness derivative also increases. This is an improvement of previous theory as the effect of leeward surface are included in the present work.
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	Computation of stiffness derivative for an unsteady delta wing with curved leading edges
title_short	Computation of stiffness derivative for an unsteady delta wing with curved leading edges
title_full	Computation of stiffness derivative for an unsteady delta wing with curved leading edges
title_fullStr	Computation of stiffness derivative for an unsteady delta wing with curved leading edges
title_full_unstemmed	Computation of stiffness derivative for an unsteady delta wing with curved leading edges
title_sort	computation of stiffness derivative for an unsteady delta wing with curved leading edges
publisher	Institute of Institutional Industrial Research
publishDate	2017
url	http://irep.iium.edu.my/61843/ http://irep.iium.edu.my/61843/ http://irep.iium.edu.my/61843/1/Paper-5-IJRRA-04-04-18.pdf
first_indexed	2023-09-18T21:27:43Z
last_indexed	2023-09-18T21:27:43Z
_version_	1777412303869706240

Computation of stiffness derivative for an unsteady delta wing with curved leading edges

Similar Items