Full Text Available

Note: Clicking the button above will open the full text document at the original institutional repository in a new window.

A discrete vortex model for the calculation of aerodynamic loads on a blade of a N-bladed helicopter rotor in rectilinear flight

Thesis (M. Ing.) -- University of Stellenbosch, 1992.

Saved in:
Bibliographic Details
Main Author: Arnold, Jacob
Other Authors: Thiart, G. D.
Format: Thesis
Language:en_ZA
Published: Stellenbosch : Stellenbosch University 2012
Subjects:
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items: A discrete vortex model for the calculation of aerodynamic loads on a blade of a N-bladed helicopter rotor in rectilinear flight