A flexible air supply hose is connected to a compressed air tank as shown in the...
A compressed-air tank holds 0.470 m^3 of air at a temperature of 283 K and a pressure of 900 kPa . What volume would the air occupy if it were released into the atmosphere, where the pressure is 101 kPa and the temperature is 305 K ?
Review of air at a temperature of A compressed-air tank holds 0.490 m 281 K and a pressure of 900 kPa. Part A What volume would the air occupy if it were released into the atmosphere, where the pressure is 101 kPa and the temperature is 305 K? 180 AEC O O ? v- [ Submit Request Answer
A tank of compressed air of volume 1.00 m3 is pressurized to 22.4 atm at T = 273 K. A valve is opened, and air is released until the pressure in the tank is 13.7 atm. How many molecules were released? Boltzmann constant is 1.38 × 10−23 J/K. How long will the air in the tank last at 22.2 m? ___min
Air flow is induced in an insulated tube of 7.16 mm diameter by a vacuum pump. Air is drawn from a room where stagnation pressure is 101 kPa (abs) and stagnation temperature 23 °C, through a smoothly contoured converging nozzle. At station (1), where the converging nozzle joins the constant area tube, the static pressure is 98.5 kPa (abs). At section (2), located some distance downstream in the constant area tube, the air temperature is 14 °C. Determine a) the...
Air flows through a converging-diverging nozzle/diffuser. Assuming isentropic flow, air as an ideal gas, and constant specific heats determine the state at several locations in the system. Solve using equations rather than with the tables. Note: The specific heat ratio and gas constant for air are given as k-14 and R-0.287 LJ/kg-K respectively, --Given Values Inlet Temperature: TI (K) - 339 Inlet pressure: P1 (kPa)=618 Inlet Velocity: VI (m/s) = 68 Area at nozzle inlet: Al (em'2)7.77 Throat area: A...
Air flows through a converging-diverging nozzle/diffuser. Assuming isentropic flow, air as an ideal gas, and constant specific heats determine the state at several locations in the system. So equations rather than with the tables. 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-- Inlet Temperature: T1 (K) = 348 Inlet pressure: P1 (kPa) = 544 Inlet Velocity: V1 (m/s) = 122 Area at nozzle inlet: A1 (cm^2) = 8.81...
Air flows through a converging-diverging nozzle/diffuser. Assuming isentropic flow, air as an ideal gas, and constant specific heats determine the state at several locations the system. Solve using equations rather than with the tables. 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-- Inlet Temperature: T1 (K) = 353 Inlet pressure: Pl (kPa) = 546 Inlet Velocity: V1 (m/s) = 61 Area at nozzle inlet: A1 (cm^2) = 7.24...
MATLAB Program Problem D 0.02 m d 0.01 m 0 P1 3.0 kPa Air Review the tank diagram above. Air flows steadily from a tank, through a hose of diameter D-0.02 m, and exits to the atmosphere from a nozzle of diameter d-0.01 m. The pressure in the tank remains constant at 3.0 KPa and the atmospheric conditions are standard temperature and pressure. Determine the flow rate at the exit and the pressure in the hose. File Submission Save your...
2.-Consider a cylindrical combustion chamber where air enters at 480 kPa with a density of 3.05 kg/m. At inlet the stagnation air temperature is 553K. Heat is added by combustion and the air exits the chamber at a Mach number of 0.4. Determine the stagnation temperature at the exit and the specific heat added to the chamber due to combustion if the chamber is assumed frictionless. Specific heat at constant pressure of air is 1.005 kJ/kg.K and the gas constant...
Air flows through a converging-diverging nozzle/diffuser. Assuming isentropic flow, air as an ideal gas, and constant specific heats determine the state at several locations in the system. Solve using equations rather than with the tables. 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-- Inlet Temperature: T1 (K) 370 Inlet pressure: P1 (kPa) = 576 Inlet Velocity: V1 (m/s) - 106 Area at nozzle inlet: A1 (cm^2) = 8.32...