Please use this identifier to cite or link to this item: http://buratest.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
Dept of Design Research Papers



Items in BURA are protected by copyright, with all rights reserved, unless otherwise indicated.