Calculation of Rotorcraft Inflow Model Coefficients Using Blade Flapping Measurements
Author:
Affiliation:
1. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.40540
Reference20 articles.
1. Rotor Wake Modeling for Flight Dynamic Simulation of Helicopters
2. Technical Note: Dynamic Inflow for Practical Applications
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