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.
|
Text (scanned version of the original print report)
185236.pdf - Published Version 13MB |
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 > Autonomous Systems and Connectivity |
| 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 |
University Staff: Request a correction | Enlighten Editors: Update this record
Deposit and Record Details
Deposit and Record Details