Unsteady Momentum Source Method for Efficient Simulation of Rotor Aerodynamics
Author:
Affiliation:
1. Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031934
Reference28 articles.
1. A review of computational techniques for rotor wake modeling
2. Modern helicopter rotor aerodynamics
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4. Effect of Wake Adaptation on Rotor Hover Simulations Using Unstructured Meshes
5. Unsteady Overset Simulation of Rotor-Airframe Interaction
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