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During an emergency launch operation to fill a missile with RP-4, the volume of a well insulated fuel storage tank is pressurized to 10.34 bar with air coming from a large external storage tank at high pressure (69 bar). the overall operation is complete as rapidly as possible. the fuel storage tank can be approximated as a right circular cylinder 12.2m tall and 3.05m in diameter and is originally filled to 90% capacity. the initial conditions in the tank are T=300K and P=1atma) comment on any safety hazards that might be encountered. especially, what would you anticipate if the inlet gas control valve were to malfunction and the gas space above the fuel were to reach full storage tank pressure (69bar)? the fuel tank has been hydrostatically tested to 276 bar.b) calculate the temperature of the gas in the tank when the pressure has reached 10.34 bar and if the valve does not function properly and the pressure in the tank reaches 69 bar. consider the air to be an ideal gas with Cp=(7/2)R
Draw the stress distribution along the walled thickness and discuss whether the composite with the applied pressure is safe or not by using von-Mises and Tresca theory.
what type of feedback data should we be collecting; in order to make sure that our MPS data, our MRP data, our Aggregate Planning, etc. are all correct?
You are designing a remote-area power supply based on a miniature wind turbine that is 20% efficient. Meteorological data indicates an average wind speed of 24 km/h at an air temperature of 10oC and pressure of 0.9 atm. The rotor has a diameter of..
Determine the magnitude of the horizontal and vertical components of the force of the water on the gate.
Determine the internal normal force, shear force, and moment at point C in the simply supported beam. Point C is located just to the right of the 1500 couple moment.
a boiling-water-type nuclear fission reactor has shut down the backup pumps have failed and emergency cooling water
If the atmospheric pressure is 90 kPa, determine the pressure inside the cylinder.
The purpose of this project is to introduce you to the application of FEA by using the ANSYS software to examine the deflection of an I-beam under a point load.
Determine the angle between his velocity vector and the line from his position to the airlock's position.
(a) Draw a schematic of the system and (b) determine if the inventor's claims are true.
Given that the nominal diameter (per print) is 15.00mm +/-0.10mm, what can be said about the expected defect rate?
Determine the velocity of shearing along the shear plane and the velocity of sliding at the tool-chip interface and find the work done per minute in shearing the metal and against the friction.
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