Study of Vortex Breakdown and Pitch up on a Compound Delta Wing

This paper discusses the calculation of mean pressure on a compound delta wing configuration and its variance to understand vortex breakdown and pitch up on the setup. The configuration of the compound delta wing being used was 50°-60°. The data was used to find the location of vortex breakdown and...

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Bibliographic Details
Main Authors:	SHIVAM, Shashi Bhushan VERMA
Format:	Article
Language:	English
Published:	National Institute for Aerospace Research “Elie Carafoli” - INCAS 2019-06-01
Series:	INCAS Bulletin
Subjects:	Compound Delta ta Wing vortex breakdown pitch up Delta wing Mean pressure
Online Access:	http://bulletin.incas.ro/files/shivam_verma_vol_11_iss_2.pdf

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spelling	doaj-497c0a4b31fe499d9b37e0736e03d65f2020-11-24T20:55:57ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282019-06-0111217117810.13111/2066-8201.2019.11.2.14Study of Vortex Breakdown and Pitch up on a Compound Delta WingSHIVAM0Shashi Bhushan VERMA1Department of Aerospace Engineering, Punjab Engineering College, Chandigarh, India, shivamkmr7@gmail.comExperimental Aerodynamics Division, National Aerospace Laboratories, Bangalore, India, sbverma@hotmail.comThis paper discusses the calculation of mean pressure on a compound delta wing configuration and its variance to understand vortex breakdown and pitch up on the setup. The configuration of the compound delta wing being used was 50°-60°. The data was used to find the location of vortex breakdown and pitch up over the compound delta wing. It was done using calibration of different pressure ports on span and chord wise location of the wing. The pressure values were then converted to Coefficient of Pressure (Cp) for proper study and comparison.http://bulletin.incas.ro/files/shivam_verma_vol_11_iss_2.pdfCompound Delta ta Wingvortex breakdownpitch upDelta wingMean pressure
collection	DOAJ
language	English
format	Article
sources	DOAJ
author	SHIVAM Shashi Bhushan VERMA
spellingShingle	SHIVAM Shashi Bhushan VERMA Study of Vortex Breakdown and Pitch up on a Compound Delta Wing INCAS Bulletin Compound Delta ta Wing vortex breakdown pitch up Delta wing Mean pressure
author_facet	SHIVAM Shashi Bhushan VERMA
author_sort	SHIVAM
title	Study of Vortex Breakdown and Pitch up on a Compound Delta Wing
title_short	Study of Vortex Breakdown and Pitch up on a Compound Delta Wing
title_full	Study of Vortex Breakdown and Pitch up on a Compound Delta Wing
title_fullStr	Study of Vortex Breakdown and Pitch up on a Compound Delta Wing
title_full_unstemmed	Study of Vortex Breakdown and Pitch up on a Compound Delta Wing
title_sort	study of vortex breakdown and pitch up on a compound delta wing
publisher	National Institute for Aerospace Research “Elie Carafoli” - INCAS
series	INCAS Bulletin
issn	2066-8201 2247-4528
publishDate	2019-06-01
description	This paper discusses the calculation of mean pressure on a compound delta wing configuration and its variance to understand vortex breakdown and pitch up on the setup. The configuration of the compound delta wing being used was 50°-60°. The data was used to find the location of vortex breakdown and pitch up over the compound delta wing. It was done using calibration of different pressure ports on span and chord wise location of the wing. The pressure values were then converted to Coefficient of Pressure (Cp) for proper study and comparison.
topic	Compound Delta ta Wing vortex breakdown pitch up Delta wing Mean pressure
url	http://bulletin.incas.ro/files/shivam_verma_vol_11_iss_2.pdf
work_keys_str_mv	AT shivam studyofvortexbreakdownandpitchuponacompounddeltawing AT shashibhushanverma studyofvortexbreakdownandpitchuponacompounddeltawing
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Study of Vortex Breakdown and Pitch up on a Compound Delta Wing

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