Engineering, 18.07.2019 00:40, skylastrusz7643
At a point upstream of the throat (the throat area is 35cm2) of a converging-diverging nozzle the properties are vi=200m/s, t=300k, and p1=125kpa. if the exit flow is supersonic, compute for the isentropic case (a) the mass flow rate and (b) a1.
Answers: 3
Engineering, 04.07.2019 18:10, meganwintergirl
Afour cylinder four-stroke in-line engine has a stroke of 160mm, connecting rod length of 150mm, a reciprocating mass of 3kg and its firing order is 1-3-4-2. the spacing between cylinders is 100mm. i. show that the engine is in balance with regard to the primary inertia forces and primary 3. a and secondary inertia couples. li determine the out of balance secondary inertia force ii. propose ways of balancing this out of balance force and discuss the challenges that will arise
Answers: 3
At a point upstream of the throat (the throat area is 35cm2) of a converging-diverging nozzle the pr...
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