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Unformatted text preview: /follows: O$/),,.3#'$#Y)8$8&$)*-#8$5'#5$'58)&$ ) $ Flight conditions: 8M∞ =*&,LL-#$11Y)kPa&$*= LL-#$8"'&58$5'#5$'58)&$ $ I#?I V6$ 4.0 p∞ = #.6 8$8, T∞ & 217 K Fuel properties: f = 0.03, qhv = 120 MJ/kg Calculate the mass flow rate through the wind tunnel. $ 8"#$ 3858)9$ Ramjet properties:W5C7$ = 358e)/At =#20#'58.'#$ @BC7$ 5*/$ ,-&%$ J#-&9)8R$ 0'#33.'#$ @( Ad /Ai 38, A 9$ 8 2 C$58$#59"$&,$Find#the&--&%)*+$3858),&*3Mtemperature (K) and Mach number at 8" $, static pressure (kPa ) static $ 5:$ Z858)&*$[$1#"I)*/$8"#$normal shock3&quo...
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This note was uploaded on 04/14/2010 for the course AEROSP 225 taught by Professor Powell during the Winter '10 term at University of Michigan.

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