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An aircraft engine is fitted with a single-sided centrifugal compressor. The aircraft flies with a speed of 230 m/s at an altitude where the pressure, pa = 0.23 bar and the temperature, Ta = 217 K (note these are static values). The intake duct of the impeller eye contains fixed vanes which give the air prewhirl of 250 at all radii. The inner and outer diameters of the eye are 18 and 33 cm respectively, the diameter of the impeller periphery is 54 cm and the rotational speed is 270 rev/s. Estimate the stagnation pressure at the compressor outlet when the massflow is 3.60 kg/s.Neglect losses in the inlet duct and fixed vanes, and assume that the isentropic efficiency of the compressor,ηcs= 0.80. Take the slip factor, σ= 0.9 and the power input factor,φ = 1.04.
Package Design Brief: Assume you are the packaging engineer for a large consumer products company. In this company, the Packaging Design Briefs are initiated by the marketing group and forwarded to the Package Engineering group.
Define dynamic viscosity, Determine the centroid, Pressure due to the height of liquid, Advantage of changing the liquid, Calculate the total moment about the hinge of the seal gate.
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Write a paper on Boyle's law and describe Compression and Combustion stroke . Also explain Charles's law and illustrate SI engine and CI engine.
To Verify the law for parallelogram of forces, law for triangle of forces and law of polygon of forces. These laws are very useful to calculate unknown forces in very short time.
What is the discharge revised discharge pressure of the compressor.
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Wind turbines are becoming more and more common as a method of energy production, wind turbines by their very nature are dynamic and are subject to and create their own internal and external kinematics and kinetics.
8 x product engineering and design review (week 2 – 12), ~3 pages per item which must contain a brief description of the product then delve into concepts such as materials selection, manufacturing methods, life cycle analysis, recyclability and overa..
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Determine maximum total bending moment (static plus dynamic) of the beam under steady-state conditions.
Determine the magnitude of the horizontal and vertical components of the force of the water on the gate.
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