Problem 1(25 points) 0, for x < 0 Consider air flowing over a surface sketched below, which is given as y= 1 -0.1x’, for

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Problem 1 25 Points 0 For X 0 Consider Air Flowing Over A Surface Sketched Below Which Is Given As Y 1 0 1x For 1 (53.85 KiB) Viewed 21 times

Problem 1(25 points) 0, for x < 0 Consider air flowing over a surface sketched below, which is given as y= 1 -0.1x’, for x 20 M = 3, P, =100 kPa, T, = 300°K. = = Problem 1.1(21 points). p! At point p , where x, = 2,find the Mach number M angle a, (in degrees), pressure Pp (kPa) and temperature T, (°K).Two red lines represent expansion waves, the blue horizontal dotted line is a reference line drawn parallel to the x axis. M, 0.5 1.5 20 2.5 3.0 -0.5 - 1.0 p 9 -15 not to scale