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3 Geometries
1 Mesh
1 Simulation setup
1 ResultAENG344 Problem 9.14 Consider a diamond-wedge airfoil such as shown in Figure 9.36, with a half-angle 10 degrees. The airfoil is at an angle of attack of 15 degree to a Mach 3 freestream. Calculate the lift and wave-drag coefficients for the airfoil
by slilbaekslilbaek
ssalehian created this project
over 4 years ago
3 Geometries 1 Mesh 1 Simulation setup 1 ResultAENG344 Problem 9.14 Consider a diamond-wedge airfoil such as shown in Figure 9.36, with a half-angle 10 degrees. The airfoil is at an angle of attack of 15 degree to a Mach 3 freestream. Calculate the lift and wave-drag coefficients for the airfoil
