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a. Challenges and knowledge gaps in the fields you chosen.
b. Major technical specification, such as sensitivity, resolution, driving voltage etc. for thestate of art technologies
c. Description of the working principle of subsystems or technologies including pictures ofthe system or subsystems
d. Design methodology used
e. Pros and cons of the existing technology from your evaluation.
Compute the slope at support A and the deflection at point B. Express the answer in terms of EI.
The absolute velocity leaving the rotor at section (2) is radial with a magnitude of 12 m/s. Determine the energy transfer per unit mass of fluid flowing through this turbine if the fluid is (a) air, (b) water.
a carpet of length x is lying on the floor. it is folded to half of its length backwards over itself. what is the new position of the centre of mass of the carpet
When these stops occur, it takes an average of 10.0 min to diagnose the problem and make repairs. Determine (a) line efficiency and (b) average actual production rate.
an ideal brayton cycle has reheat between the first and second staged turbines and regeneration following the second
calculate the joule-thomson coefficient for r-134a at a state of 140 degree f and 30 psia use this value of the j.t.c.
a 1500-n weight is attached to a small light pulley that can roll on the cable abc. the pulley and weight are held in
for each state indicate if the fluid is compressed liquid saturated mixture or superheated vapor. show the state on a
Calculate the pressure of the air in the sealed tank shown in Fig. 6.25 that would cause the velocity of flow to be 20 ft/s from the nozzle. The depth h is 10 ft.
The car travels at a constant speed of 25 m/s makes a turn on a semi-circular curve. If it takes 20s to make the semi-circular turn, determine the magnitude of the car’s acceleration during the turn.
Assume all deflections to be small (e.g., m moves approximately vertically if θ is small), and neglect gravity. Use the Extended Hamilton's Principle to derive the equations of motion and the boundary conditions for this system.
a steam turbine is limited to a maximum inlet temperature of 800.degc. the exhaust pressure is 0.0100 mpa and the
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