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Please find attached some work I need help with. I have also attached the appendix which the work says is required to complete the questions
Calculate the modulus of elasticity of the aluminium alloy. Use the modulus to determine the length of a 1.25 m bar to which a stress of 210 MPa is applied.
heat amp mass transfer incropera 6th ed prob. 5.68 asphalt pavement may achieve temperatures as high as 50 degree
Calculate the static thrusts of the rocket and turbojet engine described in the figure. The thrust T is the force necessary to prevent horizontal movement of the engine. Both engines exhaust a mass flow of 40 kg/s.
A solenoid 2.8 m long has a radius of 0.85 cm and 660 turns. It carries a current I of 2.5 A. What is the approximate magnetic field B on the axis of the solenoid?
Heat transfer to air takes place partly at constant volume and partly at constant pressure, and it amounts to 1520.4 kJ/kg. Determine (a) the fraction of heat transferred at constant volume and (b) the thermal efficiency of the cycle.
An engineer insists that a component is fully constrained with 0 DOF because 2 plates are bolted together with 4 screws (assuming one of the 2 plates is considered "grounded"). Is he / she correct? Explain why or why not using concepts discuss..
Determine the time taken for the crate to come to a rest and the distance travelled if the coefficient of dynamic friction is 0.4
minimum weight design of a variable shape three-bar truss.numerical solution using the matlab optimization toolbox
i need the answer with calculating steps and details. assignment attached as a jpeg for reference
Given a simulator or actual device, identify if a control loop is in control or out of control and identify the information used to make the decision
The acceleration due to gravity at sea level is g = 9.81 m/s2 . What is the person"s weight at sea level? The acceleration due to gravity on the moon is g = 1.62 m/s2 . What would the person weigh on the moon?
Determine (a) the exit temperature, (b) the exit relative humidity of the air, (c) the exit velocity.
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