Please use this identifier to cite or link to this item:
http://bura.brunel.ac.uk/handle/2438/2139
Title: | Stalling speeds and determination of manoeuver speed for Rogallo-winged microlight airplanes |
Authors: | Gratton, GB |
Keywords: | Rogallo;Microlight;Aeroelasticity;Flexwing |
Issue Date: | 2008 |
Publisher: | American Institute of Aeronautics and Astronautics |
Citation: | Journal of Aircraft 45(2): 723-725, Mar 2008 |
Abstract: | Rogallo-winged airplanes can display a non-square law of stall speed versus loading. This Note shows, from experimental data, the form of this relationship and how this has been used during the certification of such airplanes, through operating data and modification of either maneuver speed or the normal acceleration limits |
URI: | http://bura.brunel.ac.uk/handle/2438/2139 |
ISSN: | 0021-8669 |
Appears in Collections: | Mechanical and Aerospace Engineering Brunel Design School Research Papers |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
Stalling speeds and determination of manoeuver speed for Rogallo-winged microlight airplanes.pdf | 2.22 MB | Adobe PDF | View/Open |
Items in BURA are protected by copyright, with all rights reserved, unless otherwise indicated.