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Combustion Nozdc Exhaust Fud Exit - V - Velocity m- mass flow rate p- pressure Throat 2.4 kg/s of liquid hydrogen and 24 kg/s of liquid oxygen enter a rocket engine where they are supposed to combust. A large leak in the combustion chamber allows 13 kg/s of the mixture to escape prior to combustion. (Assume that the leak is composed of the same proportion of Hz and Oz as flow into the engine.) The remaining gases combust, and the resulting hot gas exits a 43 cm diameter nozzle at a density of 0.040 kg/m3 NOTES IMAGES DISCUSS UNITS STATS HELP Part Description Answer Chk History What is the mass flow rate of gases exiting the nozzle? 10 pts, 110% 2% try punalty Hints: 1.0 A. # tries: O Show Deals include units with answer) What is the volume flow rate of gases exiting the nozzle? (include units with answer) 10 pts, 110% B. # tries: OShow Deals - Hints: 0.0 What is the velocity of the gases exiting the nozzle? (include units with answer) 10 pts, 110% # tries: O-Show Deals 2% try ธ.nalty.

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Tota (A) mass Louw lake. o velociplz upvote

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