NAME: 1. Apply the macroscopic conservation equations to the methane combustion chamber shown below: 10/ICH om COMBUSTCH 20/four Figure 2.96 Table 2.96 Gaseous Species data" (molar basikami Species 1 M A14298K) HCOOK-H(298) 4000K) O, 1 32.00 0.000 5.427 58.192 N 201 0.000 5.129 54.507 HO 3 18.016 -57.798 6209 55592 CO 4 4401 - 94.054 7984 64344 10:04 -17.995 9.125 59.141 Units 1/18 mole) kcal/gmole) kcal/(-mole) cal/gmolek! JANAF Thermochemical Tobler,Second E.INSRDENS 27/(1970) 2 S Pure CH4 gas at 300 K, I am an pure air at 300 K, 1 atm steadily flow into the chamber from which a single stream of product gas (CO2, H2), O2, N2) emerges at 1000 K. I atm. Address the following: What is the mass flow rate of the product stream exiting the combustor ? b. Compute the chemical composition of the product gas mixture in mass fractions using STANJAN (CEA RUN) c. Compute the rate of energy needed to bring the combustion product gases to 1000 K