Question 19 5 pts A normal shock forms in the diverging section of a nozzle. Upstream of the shock, the Mach number is 2.00 and the temperature is 300 K. Assuming air is the fluid with k = 1.4, R = 0.287 kJ/kg-K, and ideal gas behavior, what is the velocity of the air immediately downstream of the shock, in m/s? TABLE 9.3 Doylu 1.000 00 0.998 92 0.992 80 0.979 35 0.958 19 0.929 78 0.895 20 0.855 73 Normal Shock Functions for an Ideal Gas with k = 1.4 M Py/ 1.00 1.000 00 1.0000 1.10 0.911 77 1.2450 120 0.842 17 1.5133 1.30 0.785 96 1.8050 1.40 0.739 71 2.1200 1.50 0.701 09 2.4583 1.60 0.668 44 2.8201 1.70 0.640 55 3.2050 1.80 0.616 50 3.6133 1.90 0.595 62 4.0450 2.00 0.577 35 4.5000 2.10 0.561 28 4.9784 2.20 0.547 06 5.4800 2.30 0.534 41 6.0050 2.40 0.523 12 6.5533 2.50 0.512 99 7.1250 2.60 0.503 87 7.7200 2.70 0.495 63 8.3383 2.80 0.488 17 8.9800 2.90 0.481 38 9.6450 3.00 0.475 19 10.333 4.00 0.434 96 18.500 5.00 0.415 23 29.000 10.00 0.387 57 116.50 00 0.377 96 T/T 1.0000 1.0649 1.1280 1.1909 1.2547 1.3202 1.3880 1.4583 1.5316 1.6079 1.6875 1.7704 1.8569 1.9468 2.0403 2.1375 2.2383 2.3429 2.4512 2.5632 2.6790 4.0469 5.8000 20.388 0.812 68 0.767 35 0.720 88 0.674 22 0.628 12 0.583 31 0.540 15 0.499 02 0.460 12 0.423 59 0.389 46 0.357 73 0.328 34 0.138 76 0.06172 0.003 04 0.0