Surface pressure model for simple delta wings at high angles of attack AIAA Paper 2001-2415

Pashilkar, A. A (2001) Surface pressure model for simple delta wings at high angles of attack AIAA Paper 2001-2415. In: 19th Applied Aerodynamics Conference, 11-14 June 2001, Anaheim, CA.

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    Abstract

    A new aerodynamic modeling approach is proposed for the longitudinal static characteristics of a simple delta wing. It captures the static variation of normal force and pitching moment characteristics throughout the angle of attack range. The pressure model is based on parametrizing the surface pressure distribution on a simple delta wing. The model is then extended to a wing/body combination where body alone data are also available. The model is shown to be simple and consistent with experimental data

    Item Type: Conference or Workshop Item (Paper)
    Additional Information: Copyright of this article belongs to AIAA
    Uncontrolled Keywords: Delta Wings;Angle Of Attack;Surface Pressure;Mathematical Modelswide-body Aircraftfighter Aircraftaerodynamic Haracteristicspressure Distribution
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Flight Mechanics and Control Division
    Depositing User: Mr. N A
    Date Deposited: 20 Feb 2006
    Last Modified: 24 May 2010 09:40
    URI: http://nal-ir.nal.res.in/id/eprint/1003

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