0 0 votes Consider a flow through a nozzle, as shown in the figure below. The air flow is steady, incompressible and inviscid. The density of air is $1.23 \: kg/m^3$. The pressure difference, $(p_1-p_{\text{atm}})$ is _________ kPa (round off to $2$ decimal places) Applications gateme-2020-set2 numerical-answers applications fluid-mechanics-and-thermal-science + – ♦go_editor 300 views answer comment Share Follow Add Sync Questions 0 reply Please log in or register to add a comment.
