An ideal turbojet ingests 192 lbm/s of air at an altitude of 22000ft it flies at a mach number of 0.88 and the compressure pressure ratio is 17 the fuel has a heating value of 17900 and the burner exit total temperature is 2350 find the developed thrust dimensionless thrust and TSFC..

When at a point two solid phase changes to one solid phase on cooling then it is known as a) eutectoid point b) eutectic point c) peritectic point d) peritectoid point

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.

Calculate the bore of a cylinder that has a stroke of 18 inches and an extension time of 6 seconds at a flow rate of 4 gal/min.