1 1 vote Air enters an adiabatic nozzle at $300$ kPa, $500$ K with a velocity of $10$ m/s. It leaves the nozzle at $100$ kPa with a velocity of $180$ m/s. The inlet area is $80 \: cm^2$. The specific heat of air $C_p$ is $1008$ J/kg.K. The exit area of the nozzle in $cm^4$ is $90.1$ $56.3$ $4.4$ $12.9$ Heat Transfer gateme-2012 fluid-mechanics-and-thermal-science heat-transfer + – Andrijana3306 349 views answer comment Share Follow Add Sync Questions 0 reply Please log in or register to add a comment.
