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Saturated liquid Refrigerant-134a at 12.0°C flows through a tube in an automobile air conditioning system at a velocity of 0.300 m/s.
The tube is 1.00 m above the ground. Determine the specific flow availability of the refrigerant in the tube when the local environment (ground state) is saturated liquid Refrigerant-134a at 0.00°C.
show that the circumferential strain measured by a transverse gage on a round bar is the same as the radial strain.
reheat where high pressure and low pressure turbines are used is added to a simple steam cycle to increase the steam
Using the transport theorem approach, derive the conservation of linear momentum equations. State all assumptions. Why the transport theorem is required in the context of aircraft dynamics?
Determine (a) the velocity of the air at the duct inlet and (b) the temperature of the air at the exit.
a bicyclist starts from rest after traveling along a straight ath a distance of 20m reaches a speed of 30kmh. find his
steam enters a nozzle operating at steady state at 20 bar temperature 280c with a velocity of 80 ms. the exit pressure
Slepian-Wolf for deterministically related sources. Find and sketch the Slepian-Wolf rate region for the simultaneous data compression of (X, Y ), where y = f (x) is some deterministic function of x.
1. Define the term compression ratio. 2. What are the assumptions made for air standard cycle?
Thirty percent of the jet passes through the slot. The rest splits symmetrically along the barrier. Calculate the horizontal force F needed to hold the barrier per unit thickness into the paper.
Derive an expression relating the torque, T, in a tension test to the shear stress at the surface, τ s, in terms of the bar diameter, D, assuming that the bar is
Using Eg s = -79.0 eV for the ground state energy of helium, cal culate the ionization energy (the energy required to remove just one electron).
Water vapor at 6 MPa, 600°C enters a turbine operating at steady state and expands adiabatically to 10 kPa. The mass flow rate is 2 kg/s and the isentropic turbine efficiency is 94.7%. Kinetic and potential energy effects are negligible. Determine..
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