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: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Transonic flow;Full potential equation;Wing body analysis
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Aerodynamics, Aerodynamics, Aerodynamics
    Depositing User: Deputy Head Poornima Narayana
    Date Deposited: 01 Aug 2006
    Last Modified: 24 May 2010 09:46
    URI: http://nal-ir.nal.res.in/id/eprint/2276

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