Model helicopter rotor rig and associated strain gauge balance for performance studies

Patil, SR and Ramaswamy, MA (1987) Model helicopter rotor rig and associated strain gauge balance for performance studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    The details of a teetering rotor model and the associated strain gage balance and calibration fixtures have been presented. Hovering results for a 1.22-m diameter teetering rotor model evaluated experimentally have been compared with the simple blade element momentum theory.13;

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Flight characteristics;Helicopter design;Models;Performance prediction;Rotors;Strain gages;Hovering;Measuring instruments; Rotor aerodynamics
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 04 Feb 2008
    Last Modified: 07 Jun 2010 16:00
    URI: http://nal-ir.nal.res.in/id/eprint/4346

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