Dynamic-stall and structural-modeling effects on helicopter blade stability with experimental correlation
Author:
Affiliation:
1. Washington University, St. Louis, Missouri 63130
2. Florida Atlantic University, Boca Raton, Florida 33431
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12058
Reference11 articles.
1. Investigation of Dynamic Stall Effects on Isolated Rotor Flap-Lag Stability with Experimental Correlation
2. Hingeless Rotor Aeroelastic Stability Analysis with Refined Aerodynamic Modeling
3. 3Sharpe, D. L. "An Experimental Investigation of the Flap-Lag-Torsion Aeroelastic Stability of a Small Scale Hingeless Helicopter Rotor in Hover," NASA TP 2546, Aviation Systems Command TR 85-A-9, Jan.1986.
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