Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis
Dynamic stall deeply affects the response of helicopter rotor blades, making its modeling accuracy very important. Two commonly used dynamic stall models were implemented in a comprehensive code, validated, and contrasted to provide improved analysis accuracy and versatility. Next, computational flu...
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Georgia Institute of Technology
2012
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| Online Access: | http://hdl.handle.net/1853/43579 |