Engineering, 14.09.2019 01:30, sanafarghal
Inlet stagnation air pressure of a two-dimensional compressor cascade is 1.0 bar and inlet stagnation temperature of 295k. for an inlet mach number of 0.75 and an inlet flow angle of 48°, the exit flow angle is measured as 16.5°. assuming the flow is isentropic, determine the mass flow rate per unit frontal area, the exit mach number and the static pressure ratio across the cascade.
Answers: 2
Engineering, 03.07.2019 14:10, volleyballfun24
If the thermal strain developed in polyimide film during deposition is given as 0.0044. assume room temperature is kept at 17.3 c, and thermal coefficient of expansion for the film and the substrate are 54 x 10^-6c^-1 and 3.3 x 10^-6c^-1respectively. calculate the deposition temperature.
Answers: 3
Engineering, 04.07.2019 18:10, redrosesxx
Water at 55c flows across a flat plate whose surface temperature is held constant at 95c. if the temperature gradient at the plate's surface for a given value of x is 18 c/mm, find a) local heat transfer coefficient. b) heat flux
Answers: 3
Inlet stagnation air pressure of a two-dimensional compressor cascade is 1.0 bar and inlet stagnatio...
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English, 01.07.2019 22:00
Mathematics, 01.07.2019 22:00