QUESTION 4
Determine the final pressure (kPa) for a gas undergoing a process from state 1 (T1 = 300 K, P1 = 129 kPa) to a temperature of T2 = 839 K if s2 - s1 = 0.903 kJ/kg-K. Assume constant specific heats as given below (DO NOT USE the ideal gas tables).
Cp = 1.135 kJ/kg-K
Cv = 0.759 kJ/kg-K
QUESTION 4 Determine the final pressure (kPa) for a gas undergoing a process from state 1...
Air goes through a polytropic process in a piston/cylinder setup. The polytropic index is n. The process starts at P1 kPa, T1 oC, and ends with a pressure of P2 kPa. Answer Questions 6-8 about this process, considering the given information in Question 6. Assume air to be an ideal gas. Let, n=1.5 P1=2.3 MPa T1= 8.9 ×102 °C P2=2.1 ×102 kPa Cp = 1.004 kJ/kg-K, Cv = 0.717 kJ/kg-K, R = 0.287 kJ/kg-K Find the final temperature, in oC...
An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio rp of 9. Heat is added to the cycle at a rate of 490 kW; air passes through the engine at a rate of 1.1 kg/s; and the air at the beginning of the compression is at P1 = 71 kPa and T1 = 0 oC. Use constant specific heats at room temperature. The properties of air at room temperature are cp =1.005 kJ/kg.K and k...
4. An ideal gas with constant specific heats undergoes a process from an initial pressure of 50 kPa and initial specific volume of 4 m^3/kg to a final pressure of 80 kPa and final specific volume of 5 m^3/kg. The mass of the carbon monoxide is 3 kg. The gas has a molar mass of 44 kg/kmol and a specific heat at constant volume of 0.98 kJ/(kg∙K). Determine the entropy change of the gas during the process in kJ/K.
Problem 1 (20 points): Consider the ideal Bra below. The compressor, turbine, and process fluid is air that can be modeled as an conditions for the operation of the cycle are known: mts: Consider the ideal Brayton cycle model for an aircraft engine as shown in the diagram sur, turbine, and nozzle are all assumed to operate with an isentropic efficiency of 100%. The that can be modeled as an ideal gas with constant specific heats. The following steady-state 7...
one question part a b c d detailed solutions please and thank you Determine the constant volume specific heat (kj/kg-K) if the constant pressure specific heat is 1.31 kj/kg-K and the specific heat ratio is 1.49 Selected Answer: [None Given] Correct Answer: 0.879 ± 1 % Question 2 Determine the change in specific enthalpy (kJ/kg) of an incompressible substance with constant specific heats given the following information. C- 4.179 k/kg-K and v 1.021E-3 m3kg T1-300.1°C,P1 -162.3 kPa T2 = 437°C...
Propane is compressed from an initial state with a pressure of 100 lbf/in2 and a quality of 0.40 to a final saturated liquid state with a temperature is 50°F. Is it possible for this process to occur adiabatically? Justify your answer. Air is contained in a rigid, well-insulated container of volume 3 m3. The air undergoes a process from an initial state with a pressure of 200 kPa and temperature of 300 K. During the process, the air receives 720...
Er<E EF E E> E) W>0) and Polytropic PathsSpcl Cases for Ideal Gas n 0 constant pressure n 1 constant temperature n k constant entropy, adiabatic (q 0) n constant volume and W<0 W 0 For air R 0.287 kJ/kg-K and k Cp/Cv 1.4 if pi 300 kPa, v, 0.861 m3/kg then T, 900 K For T Ta if pa /p 3 then va = m2/kg pv RT and (T, n/(n-1) p2 V1 For vi v if po /p1 3...
Consider a piston cylinder process in air (as an ideal gas with constant specific heats) which goes from state 1 at 1 atm, 300 K to state 2 at: 3 atm and 400K. (use k=1.4, Cp = 1.005 kJ/(kg K), Cv=0.718 kJ/(kg K), R= 0.287 kJ/(kg K)) (these are the same conditions as question 4). What must the heat transfer be (in kJ/kg), if the process takes place without entropy generation and it can be assumed the temperature at system...
A Diesel cycle has a compression ratio of 22 and begins its compression at 80 kPa and 15 C. The maximum cycle temperature is 1200°C, Utilize air-standard assumptions. The properties of air at room temperature are R: 0287 The 3 kPam2kg K p 100derd kPa-m /kg-K, Cpー1.005 kJ/kg-K, cv-0718 kJ/kg.K. and k= 1.4 Determine the thermal efficiency of this cycle using variable specific heats at room temperature. Use data from the tables The thermal efficiency of this cycle is 68.97...
Air undergoes an isentropic process from p1=1atm, T1=540R to a final state where the temperature is T2=1160R. employing the ideal gas model, determine the final pressure p2, in atm. Assume a constant specific ratio k evaluated at the mean temperature.