Development of experimental techniques for helicopter rotor performance studies.

Patil, SR and Ramaswamy, MA (1988) Development of experimental techniques for helicopter rotor performance studies. Aeronautical Society of India, Vol. 4 (3). pp. 201-209.

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Abstract

The details of teetering rotor model and the associated strain gauge balance and calibration fixtures have been presented.Hovering results for 1.22 m diameter teetering rotor model evaluated experimentally have been compared with the simple blade elementum theory.

Item Type: Article
Uncontrolled Keywords: Helicopter performance;Performance tests;Rotary wings;Test facilities;Calibrating;Hovering;Hubs;Pitching moments;Rolling moments;Strain Gages
Subjects: AERONAUTICS > Aerodynamics
Depositing User: Users 90 not found.
Date Deposited: 30 Nov 2006
Last Modified: 24 May 2010 04:23
URI: http://nal-ir.nal.res.in/id/eprint/3541

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