An investigation into the effects of aerodynamic and aeroelastic scaling parameters on model scale helicopter rotors has been conducted in the NASA Langley Transonic Dynamics Tunnel. The effect of varying Reynolds number, blade Lock number, and structural elasticity on rotor performance has been studied and the performance results are discussed herein for two different rotor blade sets at two rotor advance ratios. One set of rotor blades were rigid and the other set of blades were dynamically scaled to be representative of a main rotor design for a utility class helicopter.
Important Scaling Parameters for Testing Model-Scale Helicopter Rotors
2004
16 pages
Report
Keine Angabe
Englisch
Important Scaling Parameters for Testing Model-Scale Helicopter Rotors
British Library Conference Proceedings | 1998
|FULL-LENGTH PAPERS - Important Scaling Parameters for Testing Model-Scale Helicopter Rotors
Online Contents | 2000
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