A fuel tank for a rocket in space under a zero-g environment is rotated to keep the fuel in one end of the tank. The system is rotated at 3 rev/min. The end of the tank (point A) is 1.5 m from the axis of rotation, and the fuel level is 1 m from the rotation axis. The pressure in the nonliquid end of the tank is 0.1 kPa, and the density of the fuel is 800 kg/m3 . What is the pressure at the exit (point A)
Answers: 3
Physics, 21.06.2019 23:00
Will you chech and finish these for me, because i am stumped with them.
Answers: 1
Physics, 22.06.2019 01:30
The speed of light in a material is 0.50 c. what is the critical angle of a light ray at the interface between the material and a vacuum?
Answers: 1
Physics, 22.06.2019 09:30
The necleus of an atom is made up of what subatomic particles?
Answers: 1
Physics, 22.06.2019 10:30
Air is to be preheated by hot exhaust gases in a cross-flow heat exchanger before it enters the furnace. air enters the heat exchanger at 95 kpa and 20°c at a rate of 0.6 m^3/s. the combustion gases (cp = 1.10 kj/kg°c) enter at 160°c at a rate of 0.95 kg/s and leave at 95°c. determine the rate of heat transfer to the air and its outlet temperature.
Answers: 2
A fuel tank for a rocket in space under a zero-g environment is rotated to keep the fuel in one end...
Mathematics, 17.07.2019 07:30
History, 17.07.2019 07:30
Mathematics, 17.07.2019 07:30
History, 17.07.2019 07:30
Business, 17.07.2019 07:30
Health, 17.07.2019 07:30
Mathematics, 17.07.2019 07:30
World Languages, 17.07.2019 07:30
Geography, 17.07.2019 07:30
Computers and Technology, 17.07.2019 07:30
Biology, 17.07.2019 07:30
Social Studies, 17.07.2019 07:30
Business, 17.07.2019 07:30
Business, 17.07.2019 07:30