2. Find the specific enthalpy of air at a temperature of 54°C assume air behaves as an ideal gas....
ASAP PROBLEM 2 (29pt): Air, which behaves as an ideal gas with constant specific heats (taken as Cz»-1.005品.cv-0.718 ) undergoes a constant pressure process from 27°C and 2m to 227°C at 1MPa. kgk (a) What is the mass of the air? (b) What is the heat transfer of the air in [kJ]? Find (a)m Given (fill in missing information) State 1: State 2: Air Assumptions (fill in missing information) Air behaves as an ideal gas Cp1.005.Cy0.718 kJ kgK kJ Solution
IDEAL GAS with Compressibility Factor Z correction Problem 2) Find the specific volume of the gas in Problem 1A(=1.48ft^3/lbm) using the compressibility factor Z. IDEAL GAS STATE Problem 1) Air is at 200F and a pressure of 50 psia. Assuming ideal gas estimate the specific volume of this air at this condition. Air at a density of 1.2 kg/m3 is at a pressure of 150 Kpa. Find the temperature of the air assuming ideal gas. Find the specific volume of...
An ideal gas turbine operates using air (k=1.4) coming at 375°C and 300 kPa. Find the exit pressure (kPa) if the air exits at 125 oC. Assume the air behaves ideally, properties are constant, and the turbine operates isentropically. The correct answer is 30.8 kPa
Q21) Assume that helium behaves as an ideal monatomic gas. If 33 moles of helium undergo a temperature increase of 156 K at constant pressure, how much energy (in J) has been transferred to the helium as heat?
Assume that helium behaves as an ideal monatomic gas. If 76 moles of helium undergo a temperature increase of 245 K at constant pressure, how much energy (in J) has been transferred to the helium as heat? Round your answer to the nearest whole number.
A gas turbine receives air at temperature T1 = 827 °C and specific volume v, -0.1 m®/kg. Air exits the turbine at P2 = 3 bar and T2 = 450 °C. The volumetric flow rate of air at the inlet is 0.5 m/s. The power output on the shaft is 1900 kW. Determine: The pressure of air at the inlet (pa) in kPa [2 marks] b) The mass flow rate in kg/s [1 mark] c) Find the rate of heat...
Air experiences a 50°C drop in temperature. Given that air has a gas constant of 287 J/kg·K and a specific heat ratio of 1.4, what is the total specific enthalpy change of the air?
Assume that you have a nozzle, with air entering at 300 kPa and 67 C with a velocity of 60 m/s. The air exits the nozzle at 90 kPa and 330m/s. Do NOT make an adiabatic assumption. Instead, assume that the heat losses from the nozzle to the surroundings are 3.2 kJ/kg. The surroundings are at 20 C. Assume that air is an ideal gas with variable specific heats .a) Find the exit temperature. b) Find the entropy change for...
An ideal turbojet engine is analyzed using the cold air standard method. Given specific operating conditions determine the temperature, pressure, and enthalpy at each state, and the exit velocity. Note: The specific heat ratio and gas constant for air are given as k=1.4 and R=0.287 kJ/kg-K respectively. --Given Values-- T1 (K) = 236 P1 (kPa) = 56 V1 (m/s) = 217 rp = 11.1 rc = 1.78 a) Determine the temperature (K) at state 2. b) Determine the pressure (kPa)...
Nitrous oxide (N2O) behaves as an ideal gas and has a heat capacity at constant pressure CP = 38.6 J/K∙mol. 4.2 moles of N2O initially at 298 K are heated at constant pressure until a final temperature of 358 K is reached. (a) Calculate the enthalpy change of N2O during that process. (b) Calculate the heat transfer Q during that process. (c) Calculate the work W performed during that process. (d) Calculate the change in internal energy ΔU during that...