erativ bine engine at 310 K and 100 kPa, where mpressed to 900 kPa and 650 K. The reg ectiveness of 78 percent, and the air ente DO K. Assume constant specific heats for a nperature. The properties of air at room te
erativ bine engine at 310 K and 100 kPa, where mpressed to 900 kPa and 650 K. The reg ectiveness of 78 percent, and the air ente DO K. Assume constant specific heats for a nperature. The properties of air at room te
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
Related questions
Question
![### Required Information for Regenerative Gas Turbine Engine
Air enters the compressor of a regenerative gas turbine engine at 310 K and 100 kPa, where it is compressed to 900 kPa and 650 K. The regenerator has an effectiveness of 78 percent, and the air enters the turbine at 1400 K. Assume constant specific heats for air at room temperature. The properties of air at room temperature are:
- \( c_p = 1.005 \, \text{kJ/kg}\cdot \text{K} \)
- \( k = 1.4 \)
#### Problem Statement
For a turbine efficiency of 90 percent, determine the amount of heat transfer in the regenerator. (You must provide an answer before moving on to the next part.)
The amount of heat transfer in the regenerator is: \(\_\_\_\_\_\_\_\_\_\_\_\_\_\)_ kJ/kg.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fa85a1b76-f694-4177-a1c4-606f0e4af391%2F78ffec29-5812-46f5-993b-0d2b19dcb522%2F9hb5wv_processed.jpeg&w=3840&q=75)
Transcribed Image Text:### Required Information for Regenerative Gas Turbine Engine
Air enters the compressor of a regenerative gas turbine engine at 310 K and 100 kPa, where it is compressed to 900 kPa and 650 K. The regenerator has an effectiveness of 78 percent, and the air enters the turbine at 1400 K. Assume constant specific heats for air at room temperature. The properties of air at room temperature are:
- \( c_p = 1.005 \, \text{kJ/kg}\cdot \text{K} \)
- \( k = 1.4 \)
#### Problem Statement
For a turbine efficiency of 90 percent, determine the amount of heat transfer in the regenerator. (You must provide an answer before moving on to the next part.)
The amount of heat transfer in the regenerator is: \(\_\_\_\_\_\_\_\_\_\_\_\_\_\)_ kJ/kg.
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