the work required to compress air from 300K,, 250 kPa and 0.6m^3 to 750 kPa during an isothermal process is
the work required to compress air from 300K,, 250 kPa and 0.6m^3 to 750 kPa during...
Estimate the work necessary to compress the air in an
air-compressor cylinder from a pressure of 100 kPa to 2000 kPa. The
initial volume is 1000.
An isothermal process is to be assumed.
3. (14 points) Determine whether it is possible to compress air adiabatically from 70 kPa and 310 K to 140 kPa and 390 K. a. What is the entropy change during this process? (7 points) b. Compressor efficiency (7 points) Note: Interpolate when necessary
(a) How much work is required to compress 5.08 mol of air at 19.5°C and 1.00 atm to one-twelfth of the original volume by an isothermal process? KJ (b) How much work is required to produce the same compression in an adiabatic process ? KJ (c) What is the final pressure in part (a)? ? atm (d) What is the final pressure in part (b)? ? atm
Thermodynamics
Compare the compressor work input required to compress water isentropically from 100 kPa to 1 MPa, assuming that the water exists as (a) saturated liquid and (b) saturated vapor at the inlet state.
kPa (20) 3. An ideal Stirling cycle uses air as the working fluid. The air is at 400 K and 200 kPa at the beginning of the isothermal compression process, and heat is supplied to the air from a source at 1800 K in the amount of 900 kJ/kg.Utilizing cold air-standard assumptions, determine the maximum pressure in the cycle. c,- 1.005 kJ/kg-K, k 1.4, R 0.287 kJ/kg-K tamet sam Proeess
kPa (20) 3. An ideal Stirling cycle uses air as...
1. (3 Points) Air (as an ideal gas) is compressed in an adiabatic compressor from an initial state of 100 kPa and 300K to a final state of at 200 kPa and 600K. Determine the change in specific entropy of air during this compression process. 2. (3 Points) A heat engine operates between two temperature limits of 1300 K and 400 K. It receives 1.2 MJ of heat while producing 500 kJ of useful work. Determine: a. The exergy of...
7. An industrial turbine process requires a steady 0.5 kg/s of air at 200 kPa. This air is to be the exhaust from a specially designed turbine with inlet state 400 kPa, 400 K. The heat transfer could be obtained from a source at 500 K if necessary. This process may be assumed to be reversible and the changes in kinetic and potential energy are negligible. Air is an ideal gas, with constant specific heats, using Table A.S (a) Which...
Consider a closed Brayton cycle heat-engine. Air is compressed from 300K, 100 kPa to 580K, 700 kPa. The air is heated at the rate of 950 kJ/kg before it enters the turbine. The isentropic efficiency of the turbine is 86%. Determine: a) the fraction of the turbine shaft power used to drive the compressor, and b) the thermal efficiency of the engine. Sketch the prooess on a T-s diagram. Do the calculation first with variable specific heats and then repeat...
Air is compressed steadily by a reversible compressor from 100
kPa and 300 K to 900 kPa by a 10-kW motor. Assume air is both ideal
and has constant specific heat capacity values determined at room
temperature from Table A-2 at room temperature (300 K).
a) Determine the mass flow rate through the compressor if the
process is isentropic. ( find and identify the work per unit
mass)
b) polytropic with n = 1.2
c) isothermal
d) ideal two-stage polytropic...
A tank contains air at 0.25 bars and 300K. The volume of the tank is 3 m3. A crack on the tank causes leakage from the surroundings at 1.25 bars and 350K. What is the final temperature in the tank after equilibrium is reached and how much air leaked in during the process?