Take the densilty and pressure values at 7km, and then apply Bernoulli equation. I think this is the method to solve the problem,If there any you can proceed with that. Please do it fast ,Very urgent. Question 1: . Consider an airplane flying at a standard altitude of 7 km with a velocity of 300 m/s. At a point on the wing of the airplane, the velocity is 400 m/s. Calculate the pressure at this point
Take the densilty and pressure values at 7km, and then apply Bernoulli equation. I think this is the method to solve the problem,If there any you can proceed with that. Please do it fast ,Very urgent. Question 1: . Consider an airplane flying at a standard altitude of 7 km with a velocity of 300 m/s. At a point on the wing of the airplane, the velocity is 400 m/s. Calculate the pressure at this point
Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
Publisher:Kreith, Frank; Manglik, Raj M.
Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.5P: Evaluate the dimensionless groups hcD/k,UD/, and cp/k for water, n-butyl alcohol, mercury, hydrogen,...
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Take the densilty and pressure values at 7km, and then apply Bernoulli equation.
I think this is the method to solve the problem,If there any you can proceed with that.
Please do it fast ,Very urgent.
Question 1: . Consider an airplane flying at a standard altitude of 7 km with a velocity of 300 m/s. At a point on the wing of the airplane, the velocity is 400 m/s. Calculate the pressure at this point.
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