Extendable chord for improved helicopter rotor performance
Author:
Funder
National Natural Science Foundation of China
Science and Technology on Rotorcraft Aeromechanics Laboratory Foundation
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference20 articles.
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2. Aerodynamic parameters selection in helicopter design;Sikorsky;J. Am. Helicopter Soc.,1960
3. Influence of tip shape, chord, blade number, and airfoil on advanced rotor performance;McVeigh;J. Am. Helicopter Soc.,1984
4. A review of helicopter rotor blade tip shapes;Brocklehurst;Prog. Aerosp. Sci.,2013
5. Optimization methods applied to the aerodynamics design of helicopter rotor blades;Walsh;J. Am. Helicopter Soc.,1987
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