Part 2:Problem StatementA gas turbine power plant operates on simple and ideal cycle with air as the working fluid. The pressureratio is rp = 10, compressor inlet temperature is T₁ = 300 K and turbine inlet temperature is T3Use constant specific heat cp = 1.005K and Kair = 1.4kg.K• Create a new sheet and name it "solution 1"• Create a table for T3 from 800 to 1200 with increment of AT 50 K• Calculate compressor and turbine exit temperaturesT₂ = T₁(₂)(k-1)/k(k-1)/kT4 = T3 • (-/-)Calculate compressor work Wc, turbine work WT and heat addition occ• Calculate system efficiency7thEnergy output WT - WcEnergy InputQcc• Create a scatter chart for T3 VS nth1) Add chart title2) Add axis title and show units3) Add a proper trendline and show equation• What is the system efficiency when turbine inlet temperatures are 920 and 1140 K• Create a new sheet and name it "solution 2"• Repeat all steps for pressure ratio of r₂ = 14

Part 2: blem Statement as turbine power plant operates on simple and ideal cycle with air as the working fluid. The pressure > is rp = 10, compressor inlet temperature is T₁ = 300 K and turbine inlet temperature is T3 constant specific heat cp = 1.005 kand kair = 1.4 kg.K Create a new sheet and name it "solution 1" Create a table for T3 from 800 to 1200 with increment of AT 50 K Calculate compressor and turbine exit temperatures T₂ = T₁ (rp) (k-1)/k (k-1)/k T₁=T3 - (-²)* Calculate compressor work Wc, turbine work W, and heat addition Occ - Calculate system efficiency nth Energy output W₁ - Wc Energy Input Qcc Create a scatter chart for T3 vs 17th 1) Add chart title 2) Add axis title and show units 3) Add a proper trendline and show equation What is the system efficiency when turbine inlet temperatures are 920 and 1140 K Create a new sheet and name it "solution 2"

Part 2: blem Statement as turbine power plant operates on simple and ideal cycle with air as the working fluid. The pressure > is rp = 10, compressor inlet temperature is T₁ = 300 K and turbine inlet temperature is T3 constant specific heat cp = 1.005 kand kair = 1.4 kg.K Create a new sheet and name it "solution 1" Create a table for T3 from 800 to 1200 with increment of AT 50 K Calculate compressor and turbine exit temperatures T₂ = T₁ (rp) (k-1)/k (k-1)/k T₁=T3 - (-²)* Calculate compressor work Wc, turbine work W, and heat addition Occ - Calculate system efficiency nth Energy output W₁ - Wc Energy Input Qcc Create a scatter chart for T3 vs 17th 1) Add chart title 2) Add axis title and show units 3) Add a proper trendline and show equation What is the system efficiency when turbine inlet temperatures are 920 and 1140 K Create a new sheet and name it "solution 2"

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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