In a test experiment on a model aeroplane in wind tunnel, the flow speeds on the upper and lower surfaces of the wings are 
and 
respectively. If the wing area is 
the lift of the wing is______ N. (Given density of air 
)
Text Solution
Verified by ExpertsThe correct answer is:
CHECK THE SOLUTION.
(810)
Prepare Smarter with CGP Edu
Get practice questions, solutions, and test series in one place.
Write a Review
Share your experience with this question and solution.
Commentary
Send your comment, doubt, correction, or feedback to admin.
Similar Questions
Explore conceptually related problems
A big drop is formed by coalescing 1000 small droplets of water. The surface energy will become:
A small liquid drop of radius R is divided into 27 identical liquid drops. If the surface tension i…
A small spherical ball of radius r, falling through a viscous medium of negligible density has term…
A plane is in level flight at constant speed and each of its two wings has an area of . If the spe…
The reading of pressure meter attached with a closed pipe is . On opening the valve, water starts …
A big drop is formed by coalescing 1000 small identical drops of water. If be the total surface en…