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1. Determine the compressibility factor for methane at 20.0 MPa and 0.00C.
2. In 1879, the French physicist Emile Amagat generated experimental data in a mine shaft at Verpilleux, France, for his research on the compressibility of gases. There he used a vertical column of mercury 327 m high to measure the compressibility of nitrogen at a pressure of 430. atm. Assuming the temperature at the bottom of the mine shaft was 30.0°C, use the compressibility charts to determine the value of the compressibility factor for nitrogen under these conditions.
Linear antenna array. Linear antenna array. An array antenna is made of six identical elements, each a half-wavelength dipole, and is fed with identical currents, all in phase. Spacing of the elements is one-half wavelength. Assume the antennas ar..
a cylinder made of astm a242 steel is 50cm in diameter and 250mm long and has a wall thickness of 24mm. a round bar of
Consider a single crystal of nickel oriented such that a tensile stress is applied along a [001] direction. If slip occurs on a (111) plane and in a [101] direction, and is initiated at an applied tensile stress of 13.9 MPa (2020 psi), compute the..
air at a temperature of -7c and 1 atm pressure flows along a flat surface an idealized airfoil at a constant velocity
often the assumption is made that the flow of a certain fluid can be less than 2. if air is flowing through a tube such
a woman is sliding down an incline with a const. acceleration of a0 2.3 ms2 relative to the incline. at the same time
What is the maximum data rate possible?
0.75 kg of Refrigerant 134-a is compressed in a compressor from 160 kPa and -10°C to 1.2 Mpa and 50°C, steadily. Determine the change in flow exergy of the refrigerant during this process, if the environment is at 100 kPa and 25°C.
Considering only the moments M1 and M2, calculate the maximum tensile stress σt, the maximum compressive stress σc, and the maximum in-plane shear stress τmax at point p, which is located at support A on the side of the bracket at midheight.
Calculate the reactions Derive equations for shear and moment Draw the complete shearing force and moment diagrams,
Disregarding heat conduction through the shaft and assuming one-dimensional heat transfer, determine (a) the rate of heat transfer to the coolant, (b) the surface temperature of the shaft, and (c) the mechanical power wasted by the viscous dissipa..
Calculate the boundary-layer thickness at the exit of the wind tunnel at section 2. Also calculate the exit velocity u2.
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