An airplane has two wings, each with an area of 4.00 m^2. These wings are designed such that the air flows over the top of the wing at 245 m/s and underneath the wing at 222 m/s. Assume the density (rho) is equal to 1.29 kg/m^3, and v1 is the velocity under the wing, v2 is the velocity over the wing. Determine:
a). The differential pressure required for lift
b). The mass of the airplane such that that lift on the plane will support its weight, assuming the force from the pressure difference across the wings is directed straight upward.
Prices start at $12.99 per page (275 words) for writing and $8.5 for editing and proofreading.
Instantaneous Velocity vs. Average Velocity Introduction Average velocity is given by the change in displacement of an object ov...
Report 4 Instructions Series and Parallel Circuits Label each step prior to the photo with the step in the instructions and incl...
Suppose that a plane is traveling with airspeed of 155 miles per hour, and the wind is blowing at 54.2 miles per hour 53 degrees s...
Suppose that a plane is traveling with airspeed of 155 miles per hour, and the wind is blowing at 54.2 miles per hour 53 degrees s...
A plane weighs 2280 lbs, has a wing area of 245 ft^2, and C_L of 0.15 when alpha = 0. Assume that the force of lift is equal to th...
Position and Velocity Objectives: Students will learn how position relates to constant velocity by predicting positions and...
Don't hesitate to hire one of our best essay writers.