Uv64 a variable area diuser a 0083mconstant cross

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Unformatted text preview: 1.38&'7$ 5*/$ )3#*8'&0)9$ (c) in the &)* if the Mach number is #$30 &LL-#:$!"#$/#3)+*$0inlet, 8$9&*/)8)&*3$5'0.10. #9),)#/$53$,&--&%3M$ 8$9&*/)8)&*3M$$ 2. Consider theNUV;:K7$with Vnormal $(W57$the inlet of =$B$ ramjet below, WU a 44:Eshock at !UV64 a variable area diffuser, a $0'&0#'8)#3M$constant cross-sectional area "JV46Kand >?(+$ nozzle. The design point conditions $ ,VK:KO7$X combustor, $N isentropic are $ as ?I V T#8$0'&0#'8)#3Mspecified I...
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