Framework for the Optimisation of a Helicopter Rotor Blade with an Approximate BERP Tip
Author:
Affiliation:
1. School of Engineering; University of Liverpool; UK
2. School of Engineering; University of Glasgow; UK
Publisher
John Wiley & Sons, Ltd
Reference37 articles.
1. Brocklehurst A Duque EPN 1990 Experimental and numerical study of the British Experimental Rotor Programme blade AIAA 8th Applied Aerodynamics Conference Portland, Oregon, USA
2. Aerodynamic data reconstruction and inverse design using proper orthogonal decomposition;Bui-Thanh;AIAA Journal,2004
3. Cameron L Early JM McRoberts R 2011 Metamodel assisted multi-objective global optimisation of natural laminar flow aerofoils 29th AIAA Applied Aerodynamics Conference Honolulu, Hawaii
4. Caradonna FX Tung C 1981 Experimental and analytical studies of a model helicopter rotor in hover NASA
5. Daskilewicz MJ German BJ 2012 Observations on the topology of Pareto frontiers with implications for design decision making 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition Nashville, Tennessee, USA
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