Pu Wings at supersonic flows can be modeled as a flat plate that have constant pressure distributions across their chord. Ignoring any viscous effects determine the drag force of the wing section. Round to the full N/m and make sure you use the standard sign convention (i.e. right hand rule). Use the following data chord = 1.5 m epsilon = 5 degree angle of attack = 20.0 alpha upper surface pressure = 60,000 Pa %3D lower surface pressure = 150,000 Pa

solve using analytical way Given a single disk system that rotates as in picture. If: m₁ = 10 kg; R₁ = 15 cm; θ1=30°, m₂ = 15 kg; R₂ = 20 cm; θ₂ = 100°, m3 = 10 kg; R3 = 10 cm; θ3= 160° and Re= 12,5 cm, calculated "me" and "θe"

Use Share Sketch to create this part with one sketch. Pivot lock (dimensions are in inches. The circular features in the design are all aligned to the two centers at the base.

Determine the distance from the x-axis to the center of the hole in inches.