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 grid construction for analysis of flow past swept wings. The 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, 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 > Aeronautics (General)
    Division/Department: Aerodynamics, Aerodynamics, Aerodynamics
    Depositing User: Deputy Head Poornima Narayana
    Date Deposited: 01 Aug 2006
    Last Modified: 24 May 2010 09:47
    URI: http://nal-ir.nal.res.in/id/eprint/2364

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