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8. Plot a Rayleigh line for air on the ts plane for the following inlet conditions:...
2. An aircraft with a single turbojet engine (with an inlet area of 1 m2) is...
2. An aircraft with a single turbojet engine (with an inlet area of 1 m2) is flying at cruising condition with a flight Mach number of 0.7. The ambient temperature and pressure are 250 K and 100 kPa, respectively. The engine compressor pressure ratio is 12, and the turbine inlet temperature is 1200 K. Assume all mechanical components are operating at isentropic condition and the specific heat can be considered a constant (throughout the entire engine) of 1 kJ/(kg K)....
Ethane gas (C2H6) is burned with air. The fuel flow rate is 0.1 kg/s and the air flowrate is 2.2 ...
Ethane gas (C2H6) is burned with air. The fuel flow rate is 0.1 kg/s and the air flowrate is 2.2 kg/s. Ethane's enthalpy of formation is -84,680 kJ/kmol. Determine: a. The equivalence ratio b. Ethane's lower heating value by deriving it from enthalpy of formation data. c. The heat release rate, in kw d. The mass fraction of oxygen in the products. e. The mass of CO2 emitted per 1000 hours of operation f. The mass of fuel burned per...
A medium-size centrifugal air compressor has 32 radial blades and the inlet vanes allow air suction...
A medium-size centrifugal air compressor has 32 radial blades and the inlet vanes allow air suction with no pre. whirl. The rotor speed is 7800 rpm and the tip radius is r2 = 0.25 m. Air is sucked in at a static temperature T1 = 305 K with an absolute velocity V1 = 80 m/s and a mass flow rate of 1.65 kg/s. The total-to total efficiency of the compressor is 80% and the power input factor is w =...
Fundamentals-of-Compressible-Fluid-Dynamics Balachandran CHAPTER 4 6. A conical diffuser of 15 cm...
Fundamentals-of-Compressible-Fluid-Dynamics Balachandran CHAPTER 4 6. A conical diffuser of 15 cm has an area ratio of 4. If the pressure, temperature and velocity at the inlet section are 0.69 bar, 340 K and 180 m/s, estimate the exit pressure and exit velocity. What will be the change in impulse function. [Ans. p2 = 0.8074 bar; V2 = 45 m/s; F2 - F1 = 4167.5 N] 7. The Mach number at inlet and exit of a supersonic diffuser are 3 and...
Steam Generator air (inlet) - 320°C P. = 100 kPa th =0.5 kg/s heat exchanger -...
Steam Generator air (inlet) - 320°C P. = 100 kPa th =0.5 kg/s heat exchanger - water (inlet) T = 20°C Pw = 100 kPa m = 0.025 kg/s Problem sketch Solve with EES. Document all necessary balances The problem sketch illustrates a heat exchanger in which hot air is used to generate steam. Air enters the heat exchanger at 1a, in = 320C, Pa = 100 kPa, and ma -0.5 kg/s. Model air as an ideal gas with constant...
Fuel: 0.84C12H26+0.11C7H8+0.05C2H5OH Pressure ratio: rp = 16.7 Equivalence ratio: φ = 0.38 The fuel is a three-fuel blend of: Name Chemical Formula h¯◦f n-dodecane C12H26. −35...
Fuel: 0.84C12H26+0.11C7H8+0.05C2H5OH Pressure ratio: rp = 16.7 Equivalence ratio: φ = 0.38 The fuel is a three-fuel blend of: Name Chemical Formula h¯◦f n-dodecane C12H26. −352,100 kJ/kmol toluene C7H8 12,178 kJ/kmol ethanol C2H5OH −277,507 kJ/kmol For the inlet air conditions, use a temperature of 280 K and a pressure of 100 kPa. a) Calculate the net engine power for an air mass flow rate of 50 kg/s. • Except during combustion, assume that the working fluid is air, but account...
A single-spool turbofan engine has the following data Ambient temperature Ambient pressure BPR Overall pressure ratio...
A single-spool turbofan engine has the following data Ambient temperature Ambient pressure BPR Overall pressure ratio Fan pressure ratio Fuel heating value Turbine inlet temperature Diffuser pressure recovery factor Compressor efficiency Fan efficiency Combustion efficien Burner pressure recovery factor Turbine efficiency Nozzle efficiency Flight Mach number 288 K 101.3 kN/m2 0.7 25 3.375 44,000 kJ/kg 2000 K 0.9 0.89 0.91 0.98 0.95 0.98 1.0 0.3 Calculate 1. 2. 3. Thrust per unit mass flow rate TSFC Thermal, propulsive and overall...
Fundamentals-of-Compressible-Fluid-Dynamics Balachandra Chapter 3 7. Air at 3 bar and 300 K enter...
Fundamentals-of-Compressible-Fluid-Dynamics Balachandra Chapter 3 7. Air at 3 bar and 300 K enters a duct of varying cross-sectional area of 150m/s. at inlet scetion the area is 0.05 m2. At another section downstream of it, the fluid properties are 2 bar and 280K with a flow velocity of 250m/s, Assuming air to be perfect gas, find the internal thrust produced. H [Ans. -1586.74 N] 8. The entry conditions of air into horizontal duct are 300K 345kPa and 150 m/s the...
5. Refrigerant-134a at 700kPa, 70°C, and 8 kg/min is cooled by air in a condenser until...
5. Refrigerant-134a at 700kPa, 70°C, and 8 kg/min is cooled by air in a condenser until it exits as a saturated liquid at the same pressure. The cooling air enters the condenser at 1MPa and 10°C and leaves at 17°C at the same pressure. Determine: a) Considering only the Refrigerant as a system, the heat transfer rate of a refrigerant from the condenser in (kl/min). R-134a Tables are attached! b) The mass flow rate of the air required for cooling...
AIR HEATING/COOLING HEAT PUMP sketch of a heat pump receiving outdoor air, determine the following. Assume the heat capacity of air is 1.0 kJkg-K. (a) If the supply air mass flow rate and tempera...
AIR HEATING/COOLING HEAT PUMP sketch of a heat pump receiving outdoor air, determine the following. Assume the heat capacity of air is 1.0 kJkg-K. (a) If the supply air mass flow rate and temperature (Point 3) are 0.8 kg/s and 39.7"C, and the return air temperature (Point 4) is 22C, the heating rate of the heat pump is kW. (Express your answer to one decimal place.) itthere is NO heat reco e yurt and 25% of the air is exhausted...
2. An aircraft with a single turbojet engine (with an inlet area of 1 m2) is flying at cruising condition with a flight Mach number of 0.7. The ambient temperature and pressure are 250 K and 100 kPa, respectively. The engine compressor pressure ratio is 12, and the turbine inlet temperature is 1200 K. Assume all mechanical components are operating at isentropic condition and the specific heat can be considered a constant (throughout the entire engine) of 1 kJ/(kg K)....
Ethane gas (C2H6) is burned with air. The fuel flow rate is 0.1 kg/s and the air flowrate is 2.2 kg/s. Ethane's enthalpy of formation is -84,680 kJ/kmol. Determine: a. The equivalence ratio b. Ethane's lower heating value by deriving it from enthalpy of formation data. c. The heat release rate, in kw d. The mass fraction of oxygen in the products. e. The mass of CO2 emitted per 1000 hours of operation f. The mass of fuel burned per...
A medium-size centrifugal air compressor has 32 radial blades and the inlet vanes allow air suction with no pre. whirl. The rotor speed is 7800 rpm and the tip radius is r2 = 0.25 m. Air is sucked in at a static temperature T1 = 305 K with an absolute velocity V1 = 80 m/s and a mass flow rate of 1.65 kg/s. The total-to total efficiency of the compressor is 80% and the power input factor is w =...
Steam Generator air (inlet) - 320°C P. = 100 kPa th =0.5 kg/s heat exchanger - water (inlet) T = 20°C Pw = 100 kPa m = 0.025 kg/s Problem sketch Solve with EES. Document all necessary balances The problem sketch illustrates a heat exchanger in which hot air is used to generate steam. Air enters the heat exchanger at 1a, in = 320C, Pa = 100 kPa, and ma -0.5 kg/s. Model air as an ideal gas with constant...
A single-spool turbofan engine has the following data Ambient temperature Ambient pressure BPR Overall pressure ratio Fan pressure ratio Fuel heating value Turbine inlet temperature Diffuser pressure recovery factor Compressor efficiency Fan efficiency Combustion efficien Burner pressure recovery factor Turbine efficiency Nozzle efficiency Flight Mach number 288 K 101.3 kN/m2 0.7 25 3.375 44,000 kJ/kg 2000 K 0.9 0.89 0.91 0.98 0.95 0.98 1.0 0.3 Calculate 1. 2. 3. Thrust per unit mass flow rate TSFC Thermal, propulsive and overall...
5. Refrigerant-134a at 700kPa, 70°C, and 8 kg/min is cooled by air in a condenser until it exits as a saturated liquid at the same pressure. The cooling air enters the condenser at 1MPa and 10°C and leaves at 17°C at the same pressure. Determine: a) Considering only the Refrigerant as a system, the heat transfer rate of a refrigerant from the condenser in (kl/min). R-134a Tables are attached! b) The mass flow rate of the air required for cooling...
AIR HEATING/COOLING HEAT PUMP sketch of a heat pump receiving outdoor air, determine the following. Assume the heat capacity of air is 1.0 kJkg-K. (a) If the supply air mass flow rate and temperature (Point 3) are 0.8 kg/s and 39.7"C, and the return air temperature (Point 4) is 22C, the heating rate of the heat pump is kW. (Express your answer to one decimal place.) itthere is NO heat reco e yurt and 25% of the air is exhausted...
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