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.

Full text available as:
[img] PDF
Restricted to Registered users only

Download (800Kb)

    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: Journal Article
    Uncontrolled Keywords: Helicopter performance;Performance tests;Rotary wings;Test facilities;Calibrating;Hovering;Hubs;Pitching moments;Rolling moments;Strain Gages
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 30 Nov 2006
    Last Modified: 24 May 2010 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/3541

    Actions (login required)

    View Item