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Question 1 Saturated Steam at a Pressure of 2500 KPa and 923 K, enters a horizontal steam turbine with a velocity of 300 m/sec. Determine the enthalpy, kinetic energy and potential change. Assume a heat loss of 10KJ/kg takes place in the process. Tuskene T₂=135°C U₁ = 30m/s U₂ = 100m/s U₂ = 1800kJ/kg →2 (Exit) اد (Entry) 20 (b) Determine Work done per Unt mass of steam. in Turbure flaw. сп he ent im the

Question 1 Saturated Steam at a Pressure of 2500 KPa and 923 K, enters a horizontal steam turbine with a velocity of 300 m/sec. Determine the enthalpy, kinetic energy and potential change. Assume a heat loss of 10KJ/kg takes place in the process. Tuskene T₂=135°C U₁ = 30m/s U₂ = 100m/s U₂ = 1800kJ/kg →2 (Exit) اد (Entry) 20 (b) Determine Work done per Unt mass of steam. in Turbure flaw. сп he ent im the

Introduction to Chemical Engineering Thermodynamics
Introduction to Chemical Engineering Thermodynamics
8th Edition
ISBN:9781259696527
Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Chapter1: Introduction
Section: Chapter Questions
Problem 1.1P
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Question 1 Saturated Steam at a Pressure of 2500 KPa and 923 K, enters a horizontal steam turbine with a velocity of 300 m/sec. Determine the enthalpy, kinetic energy and potential change. Assume a heat loss of 10kJ/kg takes place in the process. , Тижено T₂=135°C U₁ = 30m/s U₂ = U₂ -1 (kuny) 100m/s ← 1800kJ/kg → 2 (Exit) (b) Determine Work done per Unt mass of steam in Turbine flaw. he enthal- e mani isor. t and ver Tab
Transcribed Image Text:Question 1 Saturated Steam at a Pressure of 2500 KPa and 923 K, enters a horizontal steam turbine with a velocity of 300 m/sec. Determine the enthalpy, kinetic energy and potential change. Assume a heat loss of 10kJ/kg takes place in the process. , Тижено T₂=135°C U₁ = 30m/s U₂ = U₂ -1 (kuny) 100m/s ← 1800kJ/kg → 2 (Exit) (b) Determine Work done per Unt mass of steam in Turbine flaw. he enthal- e mani isor. t and ver Tab
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