Data Table P1 P2 Pthroat Flow G S Frr T 1 700 5 Calculations 700 Gso 23 5 24 0 700 Goo 490 5 25 1 24 5 Calculate Th 1 (30.47 KiB) Viewed 54 times
Data Table P1 P2 Pthroat Flow G S Frr T 1 700 5 Calculations 700 Gso 23 5 24 0 700 Goo 490 5 25 1 24 5 Calculate Th 2 (28.38 KiB) Viewed 54 times
DATA TABLE P1 P2 Pthroat FLOW g/s FRR T₁ 1₂ 700 5. Calculations 700 GSO 23.5 24.0 700 Goo 490 5.€ 25.1 24.5 Calculate the following using theory: 1. Nozzle throat velocity 2. Nozzle throat diameter 700 500 3:40 5.0 25.7 25.5 400 300 5.1 24.5 26.1 300 280 5.1 26.9 24.4 3. Exit pressure 4. Exit velocity 5. Nozzle efficiency 6. Dicussion and Conclusion Discuss the experimental values obtained and their correlation with the references used 200 280 S.1 23.5 26.9
In, Nozzle undergone Tecntraple process h↑ Process But in that Acter Negal Znozzle actual Entropy Increases from process 1-2 is Icentropic process I underjors irreversible 2 to 1'.. 1-2¹ hih₂ hrh₂ h₁+ (₁2 2 Process (1-2) Apply steady flow Energy Equation. =h₂- h. Enthalphy 3. Entropy t + (₂² hi= Enthalpy h₂= Enthalpy h₁ = Enthalpy of h, 2 hre₂ = ₂²4₁² 2 J at 2 at 2! process due to Aerod Enthalpy change Isentropic Enthalpy Charge where C₁, C₂ are velocities at 1, 2, 21 Despectively
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