Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
Details
- OL Work ID
- OL11624344W
Subjects
Trailing edge flapsComputational gridsAerodynamic characteristicsBlade-vortex interactionGrid generation (Mathematics)AirfoilsNoise reductionNavier-Stokes equation