P3.50 The jet engine in Fig. P3.50 admits air at 20°C and 1 atm at (1), where A1 = 0.5 m2 and V1 = 250 m/s. The fuel-air ratio is 1:30. The air leaves section (2) at 1 atm, V2 = 900 m/s, and A2 = 0.4 m². Compute the test stand support reaction Rx needed. Solution: p1 = p/RT = 101350/[287(293)] = 1.205 kg/m³. For a CV enclosing the engine, %3D %3D %3D %3D m fuct

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Author:Sadiku, Matthew N. O.
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P3.50 The jet engine in Fig. P3.50 admits air at 20°C and 1 atm at (1), where Aj = 0.5
m2 and V1 = 250 m/s. The fuel-air ratio is 1:30. The air leaves section (2) at 1 atm, V2 =
900 m/s, and A2 = 0.4 m². Compute the test stand support reaction Rx needed.
Solution: p1 = p/RT = 101350/[287(293)] = 1.205 kg/m³. For a CV enclosing the engine,
%3D
%3D
m fuel
Combustion
chamber
R,
Transcribed Image Text:P3.50 The jet engine in Fig. P3.50 admits air at 20°C and 1 atm at (1), where Aj = 0.5 m2 and V1 = 250 m/s. The fuel-air ratio is 1:30. The air leaves section (2) at 1 atm, V2 = 900 m/s, and A2 = 0.4 m². Compute the test stand support reaction Rx needed. Solution: p1 = p/RT = 101350/[287(293)] = 1.205 kg/m³. For a CV enclosing the engine, %3D %3D m fuel Combustion chamber R,
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