Question

A Diesel cycle has a compression ratio of 12 and cut-off ratio of 2. At the...

A Diesel cycle has a compression ratio of 12 and cut-off ratio of 2. At the beginning of the isentropic-compression process, the pressure and temperature are 100 kPa and 35°C (308 K), respectively. During the constant-pressure process, heat is added to the working fluid from a reservoir at a temperature of 1760°C (2033 K). During the constant volume process, heat is rejected to the environment, which is at 30°C (303 K) and 100kPa. For the air involved, it may be assumed that Cp = 1.005 kJ/kg.K and the specific heat ratio, k = 1.4.

(i) The temperature and pressure of the gas at the end of isentropic compression are _a_ K and _b_ MPa, respectively. The temperature and pressure at the end of the heat addition are _c_ K and  _d_ MPa. (ii) The cycle efficiency is _e_ %. (iii) The maximum thermal efficiency if the cycle operating between the given reservoir temperatures is reversible is _f_ %.

Homework Answers

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
An ideal Diesel cycle has a cut off ratio of 2. The temperature of the air...
An ideal Diesel cycle has a cut off ratio of 2. The temperature of the air at the beginning and at the end of the compression process are 300 K and 900 K respectively. By utilizing constant specific heats, taking the specific heat ratio, k = 1.4, Cp = 1.005 kJ/kg K and Cv = 0.718 kJ/kg K. Determine the followings: (i) The compression ratio. [5 marks] (ii) The maximum cycle temperature. [5 marks] (iii) The amount of heat transferred...
At the beginning of the compression process of an air-standard Diesel cycle operating with a compression...
At the beginning of the compression process of an air-standard Diesel cycle operating with a compression ratio of 20, the temperature is 350 K and the pressure is 0.15 MPa. The cutoff ratio for the cycle is 1.5. Determine (a) the temperature and pressure at the end of each process of the cycle, (b) the thermal efficiency, (c) the mean effective pressure, in MPa.
An inventor proposes a four-stroke cycle running on helium. The engine has a compression ratio of...
An inventor proposes a four-stroke cycle running on helium. The engine has a compression ratio of 8 and maximum operating temperature of 1,500 K. The atmospheric conditions are temperature of 300 K and pressure of 100 kPa. The processes can be approximated as below: 1- 2 isentropic compression 2- 3 constant volume heat addition 3- 4 isentropic expansion 4- 1 constant pressure heat removal a. Plot P-v and T-s diagrams for this cycle. b. Determine state conditions at the end...
1. The compression ratio of an air powered diesel cycle is A = 18 and the...
1. The compression ratio of an air powered diesel cycle is A = 18 and the cutting ratio is B = 2.2. The pressure of the air at the beginning of the compression process is C = 94 kPa and the temperature is D = 32 ° C. Considering that the specific temperatures change with temperature (using the air standard, not the cold air standard only, that is, using the relative specific volumes from the table) and accepting the gas...
Consider a cold air-standard Diesel cycle. At the beginning of compression, 102 kPa, and 300 K....
Consider a cold air-standard Diesel cycle. At the beginning of compression, 102 kPa, and 300 K. The mass of air is 0.120 kg, the compression ratio is 16, and the cut-off ratio is 2.0 For a cold air-standard analysis use the following values: cp = 1.005 kJ/kgK, cv = 0.718 kJ/kgK, k=1.40, M=28.97 kg/kmol. Determine the following : (a) pressure at end of compression stroke, in kPa (b) temperature at end of compression stroke, in K (c) maximum temperature in...
An ideal Otto cycle has a compression ratio of 7. At the beginning of the compression...
An ideal Otto cycle has a compression ratio of 7. At the beginning of the compression process, P1 = 90 kPa, T1 = 27°C, and V1 = 0.004 m3. The maximum cycle temperature is 1147°C. For each repetition of the cycle, calculate the heat rejection and the net work production. Also, calculate the thermal efficiency and mean effective pressure for this cycle. Use constant specific heats at room temperature. The properties of air at room temperature are cp = 1.005...
In an air standard diesel cycle compression starts at 100kpa and 300k. the compression ratio is...
In an air standard diesel cycle compression starts at 100kpa and 300k. the compression ratio is 16 to 1. The maximum cycle temperature is 2031K. Determine the thermal efficiency. Please help Thank you
1) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the...
1) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the compression process, the temperature is 20°C, and the pressure is 100 kPa. The heat added is 500 kJ/kg. Determine the cycle efficiency, work output, and the heat rejected 2) An air-standard Otto cycle operates with a minimum temperature of 300 K and a maximum temperature of 1700 K. The compression ratio of the cycle is 7. At the beginning of the compression process, the...
10) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the...
10) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the compression process, the temperature is 20°C, and the pressure is 100 kPa. The heat added is 500 kJ/kg. Determine the cycle efficiency, work output, and the heat rejected. 11)An air-standard Otto cycle operates with a minimum temperature of 300 K and a maximum temperature of 1700 K. The compression ratio of the cycle is 7. At the beginning of the compression process, the pressure...
A diesel cycle has a compression ratio of 18 and an intake cutoff ratio of 3....
A diesel cycle has a compression ratio of 18 and an intake cutoff ratio of 3. At the beginning of the compression process, the working fluid is at 100 Kpa and 20 degrees C. assuming variation of the specific heats find the temperature and pressure of the air in each state, the heats of input and output per unit mass and thermal efficiency.