Steady and Unsteady Aerodynamic Modeling of Trailing Edge Flaps with Overhang and Gap Using CFD and Lower Order Models
Author:
Affiliation:
1. University of Maryland
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1071
Reference29 articles.
1. Robust Individual Blade Control Algorithm for a Dissimilar Rotor
2. Swashplateless Helicopter Rotor System with Trailing-Edge Flaps for Flight and Vibration Controls
3. Aeroelastic modeling of trailing-edge flaps with smart material actuators
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