Question

What is the enthalpy of 2 kg of hydrogen gas at 500 K and 100 kPa? Express your answer to the nearest whole number in kJ. Ent
0 0
Add a comment Improve this question Transcribed image text
Answer #1

Solution Enthalpy for idea gases (H) = m CPAT (co Hydrogen = {xr ={1390) =10.3962587 1 kg ķ -i Enthelby = 2X10:39625 x(500-27

Add a comment
Know the answer?
Add Answer to:
What is the enthalpy of 2 kg of hydrogen gas at 500 K and 100 kPa?...
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for? Ask your own homework help question. Our experts will answer your question WITHIN MINUTES for Free.
Similar Homework Help Questions
  • Calculate the enthalpy change of air, in kJ/kg, if the state changed from 99 kPa and...

    Calculate the enthalpy change of air, in kJ/kg, if the state changed from 99 kPa and 35oC to 801 kPa and 419 oC using the equation of state P(v - a) = RT where a = 0.0098 m3/kg, and compare the result to the value obtained by using the ideal gas equation of state. (5 marks

  • A piston-cylinder assembly initially contains 0.8 kg of air at 100 kPa and 300 K. It...

    A piston-cylinder assembly initially contains 0.8 kg of air at 100 kPa and 300 K. It is then compressed in a polytropic process PV3 = C to half the original volume. Assuming the ideal gas model for air and specific heat ratio is constant, k=1.4, determine (a) the final temperature, (b) work and heat transfer, each in kJ. R= 0.287 kJ/kg K. W, 82

  • Is this process possible and why? 73 Air at 500 kPa, 980 K enters a turbine...

    Is this process possible and why? 73 Air at 500 kPa, 980 K enters a turbine operating at steady state and exits at 200 kPa, 680 K. Heat transfer from the turbine occurs at an average outer surface temperature of 320 K at the rate of 40 kJ per kg of air flowing. Kinetic and potential energy effects are negligible. For air as an ideal gas with c, 1.5 kJ/kg K, determine (a) the rate power is developed in kJ...

  • J. An adiabatie gas turbine espands air at 1300 kPa and 500P C to 100 kPa and 127"C Au ers turbine through a 02-...

    J. An adiabatie gas turbine espands air at 1300 kPa and 500P C to 100 kPa and 127"C Au ers turbine through a 02-m opening with an average velocity of 40 m/s, and exhausts through a 1-m opening Detormine (a) the mass fnow rate of air through the turbine and (b) the power produced by the turbine For air, take the ideal gas constant and specific heat value at constant pressure as o Yue Determine (a) the mass flow rate...

  • An ideal gas has a gas constant R = 0.3 kJ / kg K and the...

    An ideal gas has a gas constant R = 0.3 kJ / kg K and the specific heat at constant volume is Cv = 0.7 kJ / Kg K. If the gas has a temperature change of 100 ° C. Choose the correct answer by making the corresponding calculations or justifications for each of the following cases: The change in enthalpy in KJ / kg a) 30 b) 70 c) 100 d) Insufficient information The work done is in kJ...

  • 100 kg/hr of air is compressed from 110 kPa and 255 K (where it has an...

    100 kg/hr of air is compressed from 110 kPa and 255 K (where it has an enthalpy of 489 kJ/kg) to 1000 kPa and 278 K (where it has an enthalpy of 509 kJ/kg). The exit velocity of the air from the compressor is 60 m/s. The inlet velocity is very small and can be neglected. The process is adiabatic and there is no change in height during the process. a) Label all known information on the diagram. State if...

  • Air is compressed by an adiabatic compressor from P2=100 kPa to P2=500 kPa. T2=380 K and...

    Air is compressed by an adiabatic compressor from P2=100 kPa to P2=500 kPa. T2=380 K and T2=650 K. Air is an ideal gas with variable specific heats. Determine a) The exit temperature of the air for the isentropic case. Each of the above temperatures and pressures are given as actual. b) The efficiency of the compressor.

  • A combined cycle gas turbine / vapor power plant uses the turbine exhaust as the energy...

    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 of each turbine, and the overall efficiency....

  • 3 kg of nitrogen gas initially at a temp: 295K and a pressure of 100 kPa...

    3 kg of nitrogen gas initially at a temp: 295K and a pressure of 100 kPa is compressed to a higher pressure. the internal energy change during this process is 70 kJ/kg. Determine the final temperature of the nitrogen. perform two iterations with average specific heats. Please use ideal gas law PV=nRT if possible ** Please answer both questions for quick thumbs up and comment!!! 1) 2) Find the final temp of the gas Perform two iterations using average specifc...

  • Combustion gases enter an adiabatic gas turbine at 800oC and 900 kPa and leave at 100...

    Combustion gases enter an adiabatic gas turbine at 800oC and 900 kPa and leave at 100 kPa with a low velocity. Treating the combustion gases as air (R = 0.2870 kPa*m3/kg, cp = 1.005 kJ/kg*K, k = 1.4) and assuming an isentropic efficiency of 82 percent, determine the work output of the turbine and the exit temperature.

ADVERTISEMENT
Free Homework Help App
Download From Google Play
Scan Your Homework
to Get Instant Free Answers
Need Online Homework Help?
Ask a Question
Get Answers For Free
Most questions answered within 3 hours.
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT