A P-51 Mustang (a WWII vintage plane) is tested in the large wind tunnel at NASA Ames. The aircraft has an integrated pi

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A P-51 Mustang (a WWII vintage plane) is tested in the large wind tunnel at NASA Ames. The aircraft has an integrated pi

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A P 51 Mustang A Wwii Vintage Plane Is Tested In The Large Wind Tunnel At Nasa Ames The Aircraft Has An Integrated Pi 1
A P 51 Mustang A Wwii Vintage Plane Is Tested In The Large Wind Tunnel At Nasa Ames The Aircraft Has An Integrated Pi 1 (80.19 KiB) Viewed 39 times
A P-51 Mustang (a WWII vintage plane) is tested in the large wind tunnel at NASA Ames. The aircraft has an integrated pitot-static probe. We want to test the P-51 at a flight speed of 160 mph and altitude of 40,000 ft. The wind tunnel's test section has a cross-sectional area of 5000 ft2 and a reservoir area of 100,000 ft2. What pressure is needed in the reservoir to drive this flow? Hints: Similar to the previous problem, determine if the flow can be considered incompressible. We can also assume the flow through the tunnel is a Potential Flow.
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