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Trailing-Edge Noise Measurements Using a Hot-Wire Based Coherent Particle Velocity Method
National licenceAIAA | 2006| -
Shock / Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings
National licenceAIAA | 2007| -
An Implicit-Explicit Dirichlet-based Field Panel Method for Transonic Aircraft Design
National licenceAIAA | 2002| -
Design and Wind-Tunnel Verification of Low-Noise Airfoils for Wind Turbines
National licenceAIAA | 2006|
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