Engineering, 27.10.2020 18:00, aaliyahchavez13
A C-D nozzle is supplied from an air reservoir at 1000 kPa. It has an area ratio of (Aexit/Athroat) 4. Calculate: a. The range of back pressures over which there is subsonic flow in the diverging section of the nozzle (10 points) b. The range of back pressures when the flow is at the designed supersonic Mach number at exit of the nozzle (10 points)
Answers: 2
Engineering, 04.07.2019 18:10, salazjlove
Which of the following refers to refers to how well the control system responds to sudden changes in the system. a)-transient regulation b)- distributed regulation c)-constant regulation d)-steady-state regulation
Answers: 1
Engineering, 04.07.2019 18:10, jojoangelique13
The flow rate of air through a through a pipe is 0.02 m5/s. a pitot static tube is placed in the flow. the radius of the pitot static tube is 1 mm. assuming the flow to be steady and the air to be at 300k, calculate the difference in total and static pressure if the diameter of the pipe is: (a) d 0.1 m d 0.05 m (c) d 0.01 m
Answers: 2
Engineering, 04.07.2019 18:20, luisgonz5050
Find the kinematic pressure of 160kpa. for air, r-287 j/ kg k. and hair al viscosity of air at a temperature of 50°c and an absolute (10 points) (b) find the dynamic viscosity of air at 110 °c. sutherland constant for air is 111k
Answers: 3
A C-D nozzle is supplied from an air reservoir at 1000 kPa. It has an area ratio of (Aexit/Athroat)...
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