Estimation of flap schedule and minimum drag envelope

Rajeswari, B and Prabhu, KR (1983) Estimation of flap schedule and minimum drag envelope. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    A simple method has been developed to determine the13; optimum flap deflection schedule and minimum drag envelope13; for given wing and flap geometries. The method is mainly13; based on linear theory and the optimum quot;solutionquot; is.13; determined by minirnising the lift dependent drag of the wing.The method can also be used in an inverse senso for the design of the gepmetry of plain flaps at leading and13; trailing edges.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Control flow seperation;Flap geometry;Camber
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: Poornima Narayana
    Date Deposited: 30 Aug 2006
    Last Modified: 24 May 2010 09:48

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