Edu cm 5 8838398 1 81858 wind tunnel

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Unformatted text preview: 3052 FXB (Aero), *5-$5'#5$@,86 20#'58.'#$@FGC7$,-&%$J#-&9)8R$@,8?3Ken 5*/$9'&33A3#98)&powell@umich.edu CM$ 5:$ )*$8"#$8#38$3#98)&*:$ 1:$ )*$8"#1.8"'&58:$ wind tunnel is to reproduce the conditions for a launch vehicle at an altitude $ A supersonic of 147,700 ft. A converging-diverging nozzle feeds into a test section with the following 9:$ )*$8"#$)*-#87$),$8"#$N59"$*number#'$3.8, K:4K:$ pressure of 2.4 psi, stagnation operating conditions: Mach...
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