Saturated steam at 10 bar pressure is supplied to increase the temperature of the feed natural gas from its inlet temperature of 30°C to within 15°C of the steam outlet temperature. All steam properties can be verified in the steam table, attached. Evaluate the mass flow rate of the steam supplied, if about 20% of the steam is still uncondensed at the exit. The relevant properties of Natural gas (NG) are as follows: NG Flow Rate = 1500 kMol/hour Average specific heat Capacity of NG = 40 kl/kMol.°C.

Saturated steam at 10 bar pressure is supplied to increase the temperature of the feed natural gas from its inlet temperature of 30°C to within 15°C of the steam outlet temperature. All steam properties can be verified in the steam table, attached. Evaluate the mass flow rate of the steam supplied, if about 20% of the steam is still uncondensed at the exit. The relevant properties of Natural gas (NG) are as follows: NG Flow Rate = 1500 kMol/hour Average specific heat Capacity of NG = 40 kl/kMol.°C.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

calculate
QUESTION 8 On a Mollier diagram show all the stagnation and static points required to represent the complete flow process in a diffuser Air enters a diffuser with an average velocity of 375 m/s at a temperature of 360 kPa and 470 K respectively and leaves at a stagnation pressure of 300 kPa with an average velocity of 120 m/s and a static pressure of 280 kPa. stagnation pressure and Determine (i) The static pressure and Mach number of the air at inlet (ii)The diffuser efficiency, (iii)The Mach number at exit and the overall entropy increase.
I need the answer as soon as possible
Find what is needed and make sure that the solution is correct as shown in the answer to the question
QUESTION 6 Air enters a diffuser with an averaged velocity of 360 m/s at a temperature of 340 kPa and 420 K and leaves at a stagnation pressure of 300 kPa with an averaged velocity of 120 m/s and a static pressure of 285 kPa. Determine, stagnation pressure and (i) the static pressure and Mach number of the air at inlet; (ii) the diffuser efficiency (iii the Mach number at exit and the overall entropy increase
! Required information NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Steam enters a converging nozzle at 5.0 MPa and 400°C with a negligible velocity, and it exits at 3.0 MPa. It has a nozzle exit area of 50 cm². Determine the exit velocity, mass flow rate, and exit Mach number if the nozzle is isentropic. The exit velocity is m/s. kg/s. The mass flow rate is The exit Mach number is
2. Two gaseous streams enter a combined tube in a steady flow manner and leave as a single mixture Gas A at Tube A Gas B at Tube B A= 400 cm? V= 150 m/s V=0.6 m³/kg A= 250 cm? m= 455kg/min p= 2kg/m³. Data at exit: V= 100 m/s v=0.55 m/kg Find the following: a. Speed of gas at tube B b. Mass flow rate at exitp
Specify the pipe required to carry 272.200 kg of steam per hr at 87.9 kg/cm^2 ga, 538 °C, with velocity approximately 3050 m/min
Required information Carbon dioxide enters an adiabatic nozzle at 1200 K with a velocity of 70 m/s and leaves at 400 K. Assume constant specific heats at room temperature. Determine the Mach number at the inlet. The gas constant of carbon dioxide is R = 0.1889 kJ/kg-K and k = 1.288. The Mach number at the inlet is
Problem 3 – Sparky needs helium for an experimental project. The helium is stored in a storage tank at 20°C and 300 kPa. The helium exits through a converging nozzle to the environment (100 kPa atmospheric pressure) and has 10 mm exit diameter. Determine the exit flow rate of the helium. Helium’s ratio of specific heats is 1.667. This is a compressible flow problem. Only use equations and tables from the textbook to solve this problem. Note the figures in the textbook and textbook appendices are based in air, not helium, and are not valid for this problem.