Engineering, 22.10.2019 23:50 mari8493
You are designing a supersonic inlet that uses one oblique shock followed by a normal shock and you are comparing two designs. one uses an oblique shock that turns the flow 10 degrees followed by a normal shock while the other uses an oblique shock that turns the flow 25 degrees followed by a normal shock. for a flight mach number of 2.5, which design gives the smaller drop in stagnation pressure through the two shocks?
Answers: 3
Engineering, 03.07.2019 14:10
Amass of 1.5 kg of air at 120 kpa and 24°c is contained in a gas-tight, frictionless piston-cylinder device. the air is now compressed to a final pressure of 720 kpa. during the process, heat is transferred from the air such that the temperature inside the cylinder remains constant. calculate the boundary work input during this process.
Answers: 2
Engineering, 04.07.2019 16:10
An electrical motor raises a 50kg load at a construct velencity .calculate the power of the motor, if it takes 40sec to raise the load through a height of 24m(take g =9.8n/g)
Answers: 2
Engineering, 04.07.2019 18:20
Air is compressed isentropically from an initial state of 300 k and 101 kpa to a final temperature of 1000 k. determine the final pressure using the following approaches: (a) approximate analysis (using properties at the average temperature) (b) exact analysis
Answers: 1
Engineering, 04.07.2019 18:20
Acertain flow of air (at stp) has a velocity distribution given by v i (in ft/s). if this flow is going through a 4 ft square area in the yz-plane (centered at the origin), what is the mass flow rate (in lbm/s)?
Answers: 2
You are designing a supersonic inlet that uses one oblique shock followed by a normal shock and you...
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