Static Extended Trailing Edge for Lift Enhancement ... - CFD4Aircraft
Static Extended Trailing Edge for Lift Enhancement ... - CFD4Aircraft
Static Extended Trailing Edge for Lift Enhancement ... - CFD4Aircraft
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Aerodynamic Force Measurementsin Wind TunnelsNACA0012 Model with SETE (provided by NASA LaRC):Advanced Design Wind Tunnel:Speed: 6-73 m/sTest section: 4 by 3 feetTu: 0.1-0.4%Six-component balance