Now showing items 1-2 of 2
A method for the efficient calculation of elastic rotor blade dynamic response in forward flight
(Georgia Institute of Technology, 1987-05)
Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis
(Georgia Institute of Technology, 2012-01-17)
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 ...