Computation of the aerodynamic characteristics of wings in linearised supersonic flow

Ramabhadran, S and Sridharan, R (1982) Computation of the aerodynamic characteristics of wings in linearised supersonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    For the solution of tbe linearised supersonic flow equation, an explicit numerical scheme is discussed. Using this formulation,the aerodynamic characteristics of finite finite wings are coaputed based on lifting surface theory. Some results of the study of wing-fusalage configurations using this metbod are also given.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Analogue technique;Numerical methods
    Subjects: AERONAUTICS > Aircraft Stability and Control
    AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: Deputy Head Poornima Narayana
    Date Deposited: 24 Aug 2006
    Last Modified: 24 May 2010 09:48
    URI: http://nal-ir.nal.res.in/id/eprint/2489

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