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Nostrana [21]
3 years ago
10

The working section of a transonic wind tunnel has a cross-sectional area 0.5 m2. Upstream, where the cross-section area is 2 m2

, the pressure and temperature are 4 x 105 Pa and 5°C, respectively.
Find the pressure, density and temperature in the working section at the point where the Mach number is 0.8.

Assume one-dimensional, isentropic flow.
Engineering
1 answer:
myrzilka [38]3 years ago
5 0

Answer: lol

Explanation:

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<u>Since this mass of fuel added, which is 10,166.2 kg is less than 22,300 kg which is the mass of fuel required to travel from Toronto to Edmonton, the plane therefore crashed.</u>

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