Air is travelling at a velocity of 50 fps and exits on the other side of the converging nozzle with a velocity of 200 fps. Assume incompressible flow. Calculate the pressure difference between Section A and Section B. Flow in da D 44.57 psf 40.88 psf D 48.72 psf D46.22 psf D 42.65 psf D 43.61 psf
Air is travelling at a velocity of 50 fps and exits on the other side of the converging nozzle with a velocity of 200 fps. Assume incompressible flow. Calculate the pressure difference between Section A and Section B. Flow in da D 44.57 psf 40.88 psf D 48.72 psf D46.22 psf D 42.65 psf D 43.61 psf
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![Air is travelling at a velocity of 50 fps and exits on the other side of the converging
nozzle with a velocity of 200 fps. Assume incompressible flow.
Calculate the pressure difference between Section A and Section B.
Flow in
de
O 44.57 psf
O 40.88 psf
O 48.72 psf
O 46.22 psf
O 42.65 psf
O 43.61 psf](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F101c36f6-e095-4244-9b45-be24a77d423b%2Fd02c61a5-9b59-499d-8330-acd6073708c7%2Fu348xf_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Air is travelling at a velocity of 50 fps and exits on the other side of the converging
nozzle with a velocity of 200 fps. Assume incompressible flow.
Calculate the pressure difference between Section A and Section B.
Flow in
de
O 44.57 psf
O 40.88 psf
O 48.72 psf
O 46.22 psf
O 42.65 psf
O 43.61 psf
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