The development of rotor airfoil testing in the UK

Journal of the American Helicopter Society

Volumn 46, Issue 3, 2001, Pages 210-220

  Wilby, P G ^a  

^a Westland Helicopters   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

MODELS; OPTIMIZATION; REYNOLDS NUMBER; ROTORS; STIFFNESS; TURBOMACHINE BLADES;

AIRFOIL TESTING;

AIRFOILS;

EID: 0035390640     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.46.210     Document Type: Article

References (6)

1. A description of the ARA two-dimensional pitch and heave facility, and some results from the NACA 0012 wing
2. The aerodynamic characteristics of some new RAE blade sections and their potential influence on rotor performance
3. Representation of airfoil behavior
4. Two and three-dimensional indicial methods for rotor dynamic airloads
5. An experimental investigation of the influence of a range of airfoil design features on dynamic stall onset
6. Some unsteady aerodynamic effects on helicopter rotors