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KAMARAJ COLLEGE OF ENGINEERING AND TECHNOLOGY VIRUDHUNAGAR DEPARTMENT OF MECHANICAL ENGINEERING COURSE PLAN C.a!!# III1MECH S(a++ Na"# N-Pr"a.a(ha
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COURSE O$JECTIVES 4
his )ourse will de/elop the students general =nowledge in the basi) me)hani)al design, thermodynami)s, fluid me)hani)s heat transfer, and )ombustion pro)esses found in gas turbines.
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o pro/ide a )omprehensi/e =nowledge of spa)e s)ien)e and engineering and their inter relationship. o tea)h the systems approa)h to )on)ei/ing, designing, manufa)turing, managing, and operating )ompleB spa)e systems. A basi) understanding of thermodynami) )y)les of ?et engines A basi) understanding of the )ompressible fluid flow in inlets of )ompressors and turbines. A basi) understanding of the )ombustion physi)s in )ombustion )hambers A basi) understanding of the rational behind se/eral types of ?et engines.
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he ability to analy;e ?et engines determine p ropulsion effi)ien)y and design inlets and no;;les his )ourse shows the appli)ation of engineering prin)iples to a /ariety of pra)ti)al fluid flow de/i)es, in)luding ?et engines, )ombustors, and internal )ombustion engines.
#emonstrate their =nowledge about the spe)ifi) design aspe)ts of ro)=et propulsion systems and air breathing propulsion systems su)h as turbo5?ets, turbo5fan engines, ram?ets
COURSE OUTCOME
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A signifi)ant emphasis for the )ourse is the mathemati)al modeling o f the thermodynami)s and fluid me)hani)s of the )omponents ma=ing up a gas turbine. Students go through design eBer)ises su)h as spe)ifying parti)ular gas turbines for a spe)ifi) appli)ation, and also, designing and e/ aluating spe)ifi) )omponents within the turbine and in air)raft systems. 1mphasis is pla)ed on understanding physi)al phenomena and on the use of simulation and theory to understand unsteady )ompressible flows and pressure wa/es in fluids.
Students will be able to )omplete the preliminary design for an air)raft su)h that it satisfies assigned spe)ifi)ations
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Students will be able to perform basi) )omputations of aerodynami) for)es and propulsi/e for)es, performan)e of air)raft o apply mass, momentum and energy )onser/ation prin)iples to fluid dynami)s problems.
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Analy;e )ompressible flow problems in)luding randtl5Meyer eBpansions, normal obli2ue sho)=s and heat addition to )ompressible flow problems
Students will be able to predi)t the performan)e o f ro)=et propulsion systems.
MAPPING
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M"a!uring T. +r 'ur!" u('" "6a.ua(in S-n Cur!" Ou('" 4 A signifi)ant emphasis for the )ourse is the mathemati)al modeling of the thermodynami)s and fluid me)hani)s of the )omponents ma=ing up a gas turbine. Students go through design eBer)ises su)h 2 as spe)ifying parti)ular gas turbines for a spe)ifi) appli)ation, and also, designing and e/aluating spe)ifi) )omponents within the turbine and in air)raft systems. 5 1mphasis is pla)ed on understanding physi)al phenomena and on the use of simulation and theory to understand unsteady )ompressible flows and pressure wa/es in fluids.
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