Velocity Field Above a Rotor Disk by a New Dynamic Inflow Model
Author:
Affiliation:
1. Washington University, St. Louis, Missouri 63130
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3019
Reference7 articles.
1. Finite‐State Induced‐Flow Model for Rotors in Hover and Forward Flight
2. Correlation of Measured Induced Velocities with a Finite‐State Wake Model
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