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: Monograph (Technical Report)
Uncontrolled Keywords: Flight characteristics;Helicopter design;Models;Performance prediction;Rotors;Strain gages;Hovering;Measuring instruments; Rotor aerodynamics
Subjects: AERONAUTICS > Aerodynamics
Depositing User: M/S ICAST NAL
Date Deposited: 04 Feb 2008
Last Modified: 07 Jun 2010 10:30
URI: http://nal-ir.nal.res.in/id/eprint/4346

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