Modification to the cartesian grid in 3-D potential code for flow past swept wings

Ravichandran, KS and Desai, SS and Rangarajan, R (1986) Modification to the cartesian grid in 3-D potential code for flow past swept wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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Abstract

A modification is introduced in the Cartesian grid13; construction for analysis of flow past swept wings. The13; consequent location of grid points at constant percent of local chord near the leading edge of swept wings considerably improves the computed results in this region,13; especially when the velocity distribution is peaky.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Transonic flow;Full potential equation;Wing body analysis
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
Depositing User: Users 60 not found.
Date Deposited: 01 Aug 2006
Last Modified: 24 May 2010 04:16
URI: http://nal-ir.nal.res.in/id/eprint/2276

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