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A thin plate section of an airplane is uniformly deformed 0.3 mm in one corner (dispalcement to the rigth) , 0.4 mm in one corner (displacement accendent) .the dimentions:
h = 300 mm
L = 600 mm
Calculate the shear strain at the center A withouth displacement
Air enters a THREE STAGE gas turbine at 100 kPa and 17 degree Celsius. This system uses a regenerator as well as reheating and intercooling.
Calculate the change in internal energy of the gas. Remember it is an ideal gas in a constant temperature bath.
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A cylinder is internally pressurized to a pressure of 100 MPa. This cause tangential and axial stress in the outer surface of 400 and 200 MPa respectively. Make a mohr circle representing of the stress in the outer surface. What maximum shear stress ..
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discuss whether the following situations should be modeled as closed systems or open systems. clearly define the
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air is expanded from 2000 kpa and 500c to 100kpa and 50c. assuming constant specific heats determine the change in
one hundred btu of heat are transferred directly from a thermal-energy reservoir at 1200 or to one at 600 or. calculate
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