please answer 5, 6, 7, 9, An ideal gas (Oxygen) at P1 and T1 is compressed...
please answer 1,5,6,7&9
state 2 and 3 need to be calculated with the information
provided.
--Given Values-- m (kg) = 0.4 T1 (K) = 624 P1 (bar) = 1.93 P2 (bar) = 3.0301 T3 (K) = 709 1. Determine the moles (kmol) of 02. Your Answer = 0.00125 Incorrect. 2. Determine the change in internal energy (kJ) from state 1 to state 2. Your Answer = 0 Correct! 3. Determine the work (kJ) from state 1 to state 2. Your...
Thermodynamics- Gas mixture compression
An ideal gas mixture at P1 and T1 is compressed in a piston
cylinder assembly first isothermally to P2 and then isentropically
(reversible and adiabatic) to T3. Assuming variable specific heats
(use ideal gas tables) determine the following given the properties
listed below.
--Given Values--
m_O2 (kg) = 0.38
m_N2 (kg) = 0.34
T1 (K) = 650
P1 (bar) = 1.32
P2 (bar) = 2.52
T3 (K) = 738
1. Determine the pressure (bar) at state...
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 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)= 366 Inlet pressure: P1 (kPa) = 496 Inlet Velocity: V1 (m/s) = 99 Area at inlet (cm^2) = 8.7 Mach number at the exit = 1.7 a) Determine the...
A steam power plant design consists of an ideal Rankine cycle with reheat and regeneration. Steam enters Turbine 1 at P1 and T1 at the rate of m1 and exits at P2. A fraction (y') of the steam exiting Turbine 1 is diverted to a closed feedwater heater while the remainder is reheated to T3 before entering Turbine 2. A fraction (y'') of the steam exiting Turbine 2 at P4 is diverted to an open feedwater heater while the remainder...
Air confined to one side of a rigid container divided by a partition, as shown in Fig.2.The outer side is initially evacuated.The air is initially at p1=5 bar,T1=500 K, and V1= 0.2m3. When the partition is removed, the air expands to fill the entire chamber. Measurements show that V2=2V1and p2=p1/4.Assuming the air behaves as an ideal gas, determine (a) the final temperature, in K, and (b)the heat transfer, kJ.
any help thank you
Chapter 12 Ideal Gas Mixtures and Psychrometric Applications Converting Between Mass Fraction and Mole Fraction Mass Fraction Mole Fraction m/M y, M M mf M cy, MM m/M Example 1: Determine the mf CO2 0.04 MW mix mixture molecular weight mf_N2 0.7 m mix (kg) (kg/kmol), specific volume mf_02 0.2 0.06 (m®/kg), and mole fraction for mf_H20 T(C) 40 a gas mixture given the mass P (bar) 1 fraction, temperature, pressure and volume. V(m3) Example 2:...
A proposed steam power plant design consists of an ideal Rankine cycle with reheat and regeneration. Steam enters Turbine 1 at Pl and T1 at the rate of mi and exits at P2. A fraction () of the steam exiting Turbine 1 is diverted to an open feedwater heater while the remainder is reheated to T3 before entering Turbine 2. The condenser operates at P4. Saturated liquid exits the condenser and is fed to Pump 1. The outlet of Pump...
A gas contained in a piston cylinder assembly undergoes a process from state 1 to state 2 defined by the following relationship and given properties. Determine the heat transfer in kilojoules (k) to the system. Note: Carry five decimal places in all your calculations. p"V1.26 = constant E1 533.7 kj P1 348.2 kPa V1 2 m3 E2 511.7 kj P2 171.2 kPa Selected Answer: [None Given] Correct Answer: 343.00 ± 5%
please show work for all sub parts
A combined cycle gas turbine / vapor power plant uses the turbine exhaust as the energy source for the boiler. Each power system uses a single turbine. The gas power system is modeled as an ideal air-standard Brayton cycle. The vapor power system is modeled as an ideal Rankine cycle. Given specific operating conditions determine the temperature and pressure at each state, the rate of heat transfer in the boiler, the power output...
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...