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RotaryWing Aircraft

RotaryWing Aircraft IN the theory of the rotaplane developed by Glauert ref. 20 certain terms are neglected which become important at small angles of incidence of the rotor, i.e., at high forward speed. Lock ref. 16 has removed some of the approximations in Glauert's theory and obtains the same expression for the profile drag as is given in Appendix I of reference 20, which Glauert derived by consideration of the energy account. This expression, viz., http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb030616
Publisher site
See Article on Publisher Site

Abstract

IN the theory of the rotaplane developed by Glauert ref. 20 certain terms are neglected which become important at small angles of incidence of the rotor, i.e., at high forward speed. Lock ref. 16 has removed some of the approximations in Glauert's theory and obtains the same expression for the profile drag as is given in Appendix I of reference 20, which Glauert derived by consideration of the energy account. This expression, viz.,

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Mar 1, 1940

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