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Provide the up-wind finite volume formulation for generalized continuity equation.
Illustrate buckling load of the perfect column. Why many elements of the modern aircrafts are made up of the laminated composite structure?
Write down the limitations of supercharging in an IC engine.
Illustrate over speed inspection for the typical high bypass Turbofan engine. Write down the periodic inspections performed in gas turbine engine.
Critically illustrate out the Principle and operations of “Dry Sump Lubrications System”. Illustrate out the sequence about the servicing procedure of spark plugs.
Write down the advantage of the chromium plated cylindrical barrel. Critically discuss the power check in turbofan Engine.
Write down the principle of Bosch injection system. Describe in detail.
Draw a short square column to carry the axial load of 1600kn. Use M20 concrete and 415 steel.
Write down the advantages of using robot in material handling.
Describe the spatial resolution accuracy and repeatability of Robots in detail.
Explain the different types of the Gear pumps and explain the working of the external gear, with neat sketches.
List out the significant differences between the horizontal axis and vertical axis wind energy collectors.
Explain some of the advantages of the Computer Aided Design.
What is the characteristic of the system matrix of a FEA analysis? Which information can you extract from the pivot ratio?
Explain about common facilities that are available in the solid modelling package.
Does the opening of the passenger seat windows in car decrease or increase the drug? Why? Write down the special characteristics of the industrial gas turbines.
List out some of the nomenclature of a drill bit with a diagram?
How can you make low temperature by the adiabatic demagnetization?
Illustrate out the working of the simple carburetor with appropriate sketch. What are the shortcomings of simple carburetor?
Make a distinction between fire tube boiler and water tube boiler. Write down the requirement of the alternate sources of energy.
Suppose no pre whirl and no losses in intake duct, compute the blade inlet angle at root and tip of the eye, and mach number at the tip of the eye.
Deduce thrust equation for turbojet engine.
What do you mean by bypass ratio in turbofan engine? Explain in detail why SFC in turbofan engine is lower than turbojet engine?
Illustrate the controllable errors in the measurement? Describe their causes and remedies?