Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow

In this paper the focus is on study of surface pressure distribution variation with angle of incidence and Mach number for hypersonic flow/Supersonic flow for a delta wing with leading edges which are curved. It is found that the surface pressure on the wing increases with increase in incidence ang...

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Main Authors:	Crasta, Asha, Pavithra, S, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	NOVA Science Publishers 2016
Subjects:	T175 Industrial research. Research and development
Online Access:	http://irep.iium.edu.my/53341/ http://irep.iium.edu.my/53341/ http://irep.iium.edu.my/53341/1/paper2.pdf http://irep.iium.edu.my/53341/7/53341-Estimation%20of%20surface%20pressure%20distribution%20on%20a%20delta%20wing%20with%20curved%20leading%20edges_SCOPUS.pdf

id	iium-53341
recordtype	eprints
spelling	iium-533412017-03-15T02:15:02Z http://irep.iium.edu.my/53341/ Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow Crasta, Asha Pavithra, S Khan, Sher Afghan T175 Industrial research. Research and development In this paper the focus is on study of surface pressure distribution variation with angle of incidence and Mach number for hypersonic flow/Supersonic flow for a delta wing with leading edges which are curved. It is found that the surface pressure on the wing increases with increase in incidence angle and the inertia level. Results are compared for M = 8.7, 10, and 17 for delta wing with leading edge straight and curved and the results are found to be in good agreement with existing theories. NOVA Science Publishers 2016 Article PeerReviewed application/pdf en http://irep.iium.edu.my/53341/1/paper2.pdf application/pdf en http://irep.iium.edu.my/53341/7/53341-Estimation%20of%20surface%20pressure%20distribution%20on%20a%20delta%20wing%20with%20curved%20leading%20edges_SCOPUS.pdf Crasta, Asha and Pavithra, S and Khan, Sher Afghan (2016) Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow. International Journal of Energy, Environment, and Economics, 24 (1). pp. 67-73. ISSN 1054-853X http://www.novapublishers.com
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	T175 Industrial research. Research and development
spellingShingle	T175 Industrial research. Research and development Crasta, Asha Pavithra, S Khan, Sher Afghan Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
description	In this paper the focus is on study of surface pressure distribution variation with angle of incidence and Mach number for hypersonic flow/Supersonic flow for a delta wing with leading edges which are curved. It is found that the surface pressure on the wing increases with increase in incidence angle and the inertia level. Results are compared for M = 8.7, 10, and 17 for delta wing with leading edge straight and curved and the results are found to be in good agreement with existing theories.
format	Article
author	Crasta, Asha Pavithra, S Khan, Sher Afghan
author_facet	Crasta, Asha Pavithra, S Khan, Sher Afghan
author_sort	Crasta, Asha
title	Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
title_short	Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
title_full	Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
title_fullStr	Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
title_full_unstemmed	Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
title_sort	estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow
publisher	NOVA Science Publishers
publishDate	2016
url	http://irep.iium.edu.my/53341/ http://irep.iium.edu.my/53341/ http://irep.iium.edu.my/53341/1/paper2.pdf http://irep.iium.edu.my/53341/7/53341-Estimation%20of%20surface%20pressure%20distribution%20on%20a%20delta%20wing%20with%20curved%20leading%20edges_SCOPUS.pdf
first_indexed	2023-09-18T21:15:29Z
last_indexed	2023-09-18T21:15:29Z
_version_	1777411534010449920

Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow

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