Problem 1: Consider a flying wing with a NACA 2412 airfoil, an aspect atio of 10, and a wing area of 20 m2. Assume the span efficiency factor e =e= .9, and the Reynolds number 5.7 x 10. a) standard sea-level conditions. If the wing angle of attack is at 4-deg, compute Ct. and Cp at b) compute the lift L and the total drag D on the airnlane If the pressure altitude is 8 km and the flight velocity is 100 m/s,
Fluid Pressure
The term fluid pressure is coined as, the measurement of the force per unit area of a given surface of a closed container. It is a branch of physics that helps to study the properties of fluid under various conditions of force.
Gauge Pressure
Pressure is the physical force acting per unit area on a body; the applied force is perpendicular to the surface of the object per unit area. The air around us at sea level exerts a pressure (atmospheric pressure) of about 14.7 psi but this doesn’t seem to bother anyone as the bodily fluids are constantly pushing outwards with the same force but if one swims down into the ocean a few feet below the surface one can notice the difference, there is increased pressure on the eardrum, this is due to an increase in hydrostatic pressure.
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