Individual Blade Rotor Model for Use in Inverse Simulation. Internal Report No 9604

Rutherford, S. and Thomson, D. (1996) Individual Blade Rotor Model for Use in Inverse Simulation. Internal Report No 9604. Technical Report. Department of Aerospace Engineering, University of Glasgow.

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Abstract

Summary: The individual blade rotor model, “Hibrom” has been developed for use in inverse simulation of a helicopter. This report details the modelling assumptions made and the equations required to calculate the forces and moments produced by the main rotor.

Item Type:Research Reports or Papers (Technical Report)
Status:Published
Glasgow Author(s) Enlighten ID:Thomson, Dr Douglas
Authors: Rutherford, S., and Thomson, D.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
Publisher:Department of Aerospace Engineering, University of Glasgow
Copyright Holders:Copyright © 1996 Department of Aerospace Engineering, University of Glasgow
Publisher Policy:Reproduced with the permission of the Department

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