Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft
Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft
Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft
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Figure 5: Influence of the pseudo time tolerance on the lift coefficient loop for the<br />
pitch<strong>in</strong>g case at six degrees mean <strong>in</strong>cidence <strong>and</strong> an amplitude of six degrees.