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The compound helicopter configuration and the helicopter speed trap

The compound helicopter configuration and the helicopter speed trap Explains the origins of rotor aerodynamic limits for helicopters including retreating and advancing blade limits. Examines the compounding of a helicopter for higher forward speed and reports the conclusions of a student project to design a rotorcraft capable of 300 knots and carrying a payload of 30 passengers. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

The compound helicopter configuration and the helicopter speed trap

Simon Newman
Aircraft Engineering and Aerospace Technology , Volume 69 (5): 7 – Oct 1, 1997
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Publisher
Emerald Publishing
Copyright
Copyright © 1997 MCB UP Ltd. All rights reserved.
ISSN
0002-2667
DOI
10.1108/00022669710177363
Publisher site
See Article on Publisher Site

Abstract

Explains the origins of rotor aerodynamic limits for helicopters including retreating and advancing blade limits. Examines the compounding of a helicopter for higher forward speed and reports the conclusions of a student project to design a rotorcraft capable of 300 knots and carrying a payload of 30 passengers.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Oct 1, 1997

Keywords: Aerospace engineering; Design; Tests

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