Elevator Hinge moment studies over generic winged body configuration

Rajan, Kurade and Sampath, Rao (2011) Elevator Hinge moment studies over generic winged body configuration. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), 16-18 November 2011, Bangalore.

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    Abstract

    Elevator hinge moment measurements have been carried out on a generic wing body configuration through wind tunnel tests. Tests have been carried out at subsonic and transonic Mach numbers in the angles of attack range -4° to 24°. Maximum hinge moment coefficient occurs in the transonic region as expected. Positive deflections of elevator produce higher elevator hinge moment coefficient compared to that of negative deflections. Elevator hinge moment coefficient is linear with elevator deflection up to ±10° and angles of attack up to 10°.

    Item Type: Conference or Workshop Item (Paper)
    Uncontrolled Keywords: Elevator, Hinge moment, Winged-body, Subsonic, Transonic
    Subjects: ASTRONAUTICS > Astrodynamics
    Division/Department: National Trisonic Aerodynamic Facility, National Trisonic Aerodynamic Facility
    Depositing User: Ms Indrani V
    Date Deposited: 07 Dec 2011 13:25
    Last Modified: 07 Dec 2011 13:25
    URI: http://nal-ir.nal.res.in/id/eprint/10113

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