Problem 33 Perfect Taidespands Twtionless Rocket Norrle Stagnatxe Conditions Po 600 Psia Q29409555

Problem . (33%) A perfect taidespands in a twtionless rocket norrle from stagnatxe conditions Po- 600 psia. To -5000 degrees Rankine (RI, e ambient peessure of I3 psia If the espansion is isenteupic, Determise the follawing ceaditiens at the final pressures (a) Exit Velocity, Exit Mach Namber, Exit Temperature b)Exit Aea per unit mass flow (c) How does the exit flow arca compare with the throat area for a given mass flow The specific heats ratio is 1.4 and the molecular weight of the fluid is 30 Caloric value (LCV.) offet 43×10′ ?1g Semmary of Useel Conversian Factars Feree: I Newton (N)-I kgmsee 0.102 kgt Ikgf-9.81N Werk Energy er Heat: 1 oule )-1Nm-0239 cal-2.7778×10 kWbrI cal-4.1843 1.1622x 10 KW hr: 1 kWhr-86×10 kcal: Power: I wam-1 Jse-0.86 kcal Thorsepower hp)-0.1757 kcalise 735.3 wat 1&-1000 watts-860 kcalh Specific beat 1kcal kg-“K-4184 kngX: G?content (R)-287 Ag-X (fr air) or gas Show transcribed image text