Role of aeroelasticity in helicopter design

Vepa, Ranjan (1978) Role of aeroelasticity in helicopter design. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    The author offers a personal perspective on how rotocraft aeroelasticity fits into the design of a modern helicopter rotocraft aeroelasticity can be used with advantage towards the design of a modern helicopter a re reviewed.for extensive software for purposes of simulation is The manner in which recent developments in the need emphasized.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aeroelasticity;Helicopters;Design
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Propulsion Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 03 Nov 2006
    Last Modified: 24 May 2010 09:52
    URI: http://nal-ir.nal.res.in/id/eprint/3186

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