2 A convergent-divergent nozzle with an exit-to-throat area ratio of 1.616 has exit and reservoir pressures equal to 0.9

[answerhappygod]

2 A Convergent Divergent Nozzle With An Exit To Throat Area Ratio Of 1 616 Has Exit And Reservoir Pressures Equal To 0 9 1 (27.45 KiB) Viewed 29 times

2 A convergent-divergent nozzle with an exit-to-throat area ratio of 1.616 has exit and reservoir pressures equal to 0.947 atm and 1.0 atm. respectively. Assuming isentropic flow through the nozzle, calculate the mass flow through the nozzle when the reservoir temperature is 297 K and the throat area is 0.3 m2. The flow is not choked. (Round the final answer to two decimal places.) The table for isentropic filow properties is given below. 1 points <E 8 04.06.09 0.101001 0.1012-01 0.101401 10+91010 0.2200+00 0.240000 0.2600+00 0.280000 0.100)+00 0.3200+00 0.540000 0.160000 0.380000 0.000000 + Book 0.103401 0.1041 +01 0.101101 0.105601 0.106401 0.107401 0.1081+01 0.109401 01105+01 0.111701 0.1024+01 0.1029 +01 0.1034 +01 0.1000+01 0.1046 +01 0.105201 0.1059+01 0.100601 0.1074 +01 0.1082 +01 0.1018 01 0.102001 0.1023 +01 0.102601 0.2708 +01 0.249601 0.2317 +01 0.2166 +01 0.2035 +01 0.1922 +01 0,1823 +01 0.1736-01 0.165901 0.1590+01 10+60010 Hint The mass flow through the nozzle is 0.103201 kg/s. Print References