Just use results from Test No. 1 and other info provided.
The swept volume of the cylinder is calculated using the given bore and the stroke. Since there are two cylinders, it is multiplied by two. Density of air at inlet of compressor can be obtained. The volume flow rate can be calculated as the swept volume is known and the RPM of the compressor is also known. Once volume flow rate is known, the mass flow rate can be calculated. The given electrical power is the actual work or actual power supplied and it can be converted to horsepower. The isentropic and isothermal process are represented on the TS chart. The isentropic power and the isothermal power can be computed. The isentropic efficiency can also be computed as the ratio of isentropic power to the actual power (which is supplied by motor). Similarly, isothermal efficiency will be the ratio of isothermal power to the actual power. Finally, the volumetric efficiency will be the ratio of swept volumetric flow rate to the actual volumetric flow rate. The actual volumetric flow rate can be obtained as the actual power supplied is given (which is the power of motor).
Just use results from Test No. 1 and other info provided. Air box orifice =15mm Atmospheric...
A one stage axial air compressor consists of a rotor and a stator, it has a mean diameter of Im for the rotor and a rotational speed of 7645 RPM. Furthermore: Mass flow rate is 50 kg/s .Inlet static temperature and pressure of Ti 276 K and Pi 85 kPa. .Inlet stagnation temperature and pressure of Toi 290 K and Poi 101.3 kPa. .Inlet absolute velocity C1 166.5 m/s Rotor exit static density (p2) equals to 1.3kg/m3 Axial component of...
The centrifugal compressor shown here compresses air from 100 kPa, 27 °C to 600 kPa. This compressor has an isentropic efficiency of 85%. What is the air temperature at the compressor outlet and how much power does it require if the air volumetric flow rate is 9 m3/min at the compressor inlet? ideal has-hi 1 halt hasthi K- K TI OUT CH 300 =.599 Tas AR ENTERS f1technical.net .S99T25=100
Use a simple Brayton cycle gas turbine as the baseline for the following questions. Use a cold-air-standard analysis (R=0.287 kJ/kg-K, k=Cp/Cv=1.40, Cp= (k/(k-1))*R = 1.0045 kJ/kg-K) with the following specifications: Use a simple Brayton cycle gas turbine as the baseline for the following questions. Use a cold-air-standard analysis (R=0.287 kJ/kg-K, k=Cp/Cv=1.40, Cpr (k/(k-1))*R = 1.0045 kJ/kg-K) with the following specifications: Mass Inlet Press. Pressure Turbine Isentropic Eff Neglect combustion chemistry Flowrate T p Ratio Inlet T Comp Turb Neglect minor...
A motor car gas turbine unit has two centrifugal compressors in series giving an overall pressure ratio of 6/1. The air leaving the HP compressor passes through a heat exchanger before entering the combustion chamber. The expansion is in two turbine stages, the first stage driving the compressors and the second stage driving the car through gearing. The gases leaving the LP turbine pass through the heat exchanger before exhausting to the atmosphere. The HP turbine inlet temperature is 800...
System Model: Automotive Air Conditioning System Outside Air Temp: 45 oC Car Interior Air Temp: 22 oC Heat Load = 4.2 kJ/sec rate at which heat must go in to the air conditioner to be removed from the car’s interior Refrigerant: R134a HINT: Heat enters an air conditioning system where? Refrigerant 134a … - leaves the evaporator coil and enters the compressor as a saturated vapor at the evaporator pressure of 2.8 bars. - It leaves the compressor at...
The solution belongs to the 1st question, i need the solution for the 2nd question. 1. A single cylinder 1.6 lt, spark ignition engine is operating on the ideal Otto cycle at a compression ratio of 9. The ambient air around the engine is at 1 bar and 20 °C and the fuel consumption of the engine is 13 L/h gasoline at 5600 rpm. Evaluate a. The highest pressure and temperature in the cylinder throughout the cycle b. Net work...