Q₁) In an ideal otto cycle engine, the temperature and Pressure at the beginning of Compression are 43°C 100 kpa respectively and the temperature at the end of adiabatic Compression is 3232. if the temperature at the end of Gnstant Volume heat addition is 1500°C calculate: (a) the Compression ratio, (b) the air- standard efficiency, (c) the temperature and pressure at the end of adiabatic expansion. Assume Yas 1.4 Por air
Q₁) In an ideal otto cycle engine, the temperature and Pressure at the beginning of Compression are 43°C 100 kpa respectively and the temperature at the end of adiabatic Compression is 3232. if the temperature at the end of Gnstant Volume heat addition is 1500°C calculate: (a) the Compression ratio, (b) the air- standard efficiency, (c) the temperature and pressure at the end of adiabatic expansion. Assume Yas 1.4 Por air
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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![Home works
Q₁) In an ideal otto cycle engine, the temperature
and Pressure at the beginning of Compression are 43 °C
100 kpa respectively and the temperature at the end
of adiabatic Compression is 323%. if the temperature
at the end of Gnstant Volume heat addition is 1500°C
Calculate: (a) the Compression ratio, (b) the air-
standard efficiency, (c) the temperature and pressure
at the end of adiabatic expansion. Assume Yas 1.4 for
air.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F5bedc1a8-f17e-44ba-a12f-03ad4a95e209%2F2e229d97-9241-4c83-ba71-cc82a2e2fd49%2F553mhkp_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Home works
Q₁) In an ideal otto cycle engine, the temperature
and Pressure at the beginning of Compression are 43 °C
100 kpa respectively and the temperature at the end
of adiabatic Compression is 323%. if the temperature
at the end of Gnstant Volume heat addition is 1500°C
Calculate: (a) the Compression ratio, (b) the air-
standard efficiency, (c) the temperature and pressure
at the end of adiabatic expansion. Assume Yas 1.4 for
air.
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