MTech Propulsion Syllabus

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    Indian Institute of Space Science and TechnologyThiruvananthapuram

    M.Tech. Aerospace Engineering (Propulsion) Curriculum

    SEMESTER I

    Code Course Title L T P C

    AE611 Advanced Fluid Mechanics 4 4

    AE612 Fundamentals of Combustion 4 4

    AE613 Compressible Flow 4 4

    AE614 Advanced Heat Transfer 4 4

    AE615 Seminar I 1

    Total 16 17

    SEMESTER II

    Code Course Title L T P C

    AE621 Elective I 3 3

    AE622 Elective II 3 3

    AE623 Elective III 3 3

    AE624 Elective IV 3 3

    AE625 Elective V 3 3

    AE626 Seminar 2

    Total 15 17

    SEMESTER III

    Code Course Title L T P C

    AE631 Project Work - Stage I 18

    Total 18

    SEMESTER IV

    Code Course Title L T P C

    AE641 Project Work - Stage II 18

    Total 18

    Total credits = 70

    List of Electives

    Computational Fluid Dynamics

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    Measurements in Fluid and Thermal Sciences

    Boiling and Condensation

    Aerospace Propulsion

    Turbomachines

    Shockwave Dynamics

    Hypersonic Air-Breathing Propulsion

    Micro-and Nano-scale Heat Transfer

    Cryogenic Engineering

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    Indian Institute of Space Science and TechnologyThiruvananthapuram

    Course Syllabus for M.Tech. Aerospace Engineering (Propulsion)

    SEMESTER I

    AE611 ADVANCED FLUID MECHANICS 4 credits

    Eulerian and Lagrangian approach fluid kinematics; material derivative, rotation, deformation Reynoldstransport theorem physical conservation laws integral and differential formulations Navier-Stokes and energyequations exact solution of Navier-Stokes equations; steady and unsteady flows waves in fluids (potential flowformulation) boundary layer theory; Blasius solution, Falkner-Skan solutions, momentum integral approach hydrodynamic stability turbulent flows; time-averaged equations closure problem mixing-length theory lawof the wall.

    References:

    White, F. M., Viscous Fluid Flow, 3rd ed., McGraw-Hill (2006).1.

    Panton, R. L., Incompressible Flow, 3rd ed., John Wiley (2005).2.

    Kundu, P. K. and Cohen, I. M., Fluid Mechanics, 3rd ed., Academic Press (2004).3.

    Leal, L. G., Advanced Transport Phenomena, Cambridge Univ. Press (2007).4.

    Muralidhar, K. and Biswas, G., Advanced Engineering Fluid Mechanics, 2nd ed., Narosa (2005).5.

    Schlichting, H. and Gersten, K., Boundary Layer Theory, 8th ed., McGraw-Hill (2001).6.

    AE612 FUNDAMENTALS OF COMBUSTION 4 credits

    Combustion and thermochemistry fuels chemical kinetics and mechanisms reacting flows modeling of

    reacting flows premixed flames detonation and explosion diffusion flames spray combustion introductionto turbulence turbulent premixed flames turbulent non-premixed flames combustion instability.

    References:

    Turns, S. R., An Introduction to Combustion, 2nd ed., McGraw-Hill (2000).1.

    Glassman, I. and Yetter, R. A., Combustion, 4th ed., Elsevier (2008).2.

    Kuo, K. K., Principles of Combustion, 2nd ed., John Wiley (2005).3.

    Warnatz, J., Maas, U., and Dibble, R. W., Combustion 4th ed., Springer (2006).4.

    Law C. K., Combustion Physics, Cambridge Univ. Press (2006).5.

    Lefebvre A. H., Gas Turbine Combustion, Taylor & Francis (1999).6.

    AE613 COMPRESSIBLE FLOW 4 credits

    1-D gas dynamics: governing equations isentropic flow with area change, area-Mach number relations R-Hequations normal shocks.

    1-D wave motion: wave propagation simple and finite waves Reimann shock tube problem 2-D waves,governing equations oblique shocks, charts, shock polar and pressure deflection diagrams Prandtl-Meyerexpansion waves reflection and interaction of waves supersonic free jets.

    Linearized flow: subsonic flow Goethert's and Prandtl-Glauert rules hodograph methods supersonic flow supersonic thin airfoils 2-D airfoils Method of characteristics, the compatibility equation applications,supersonic nozzle design generalised one-dimensional flow, working equations influence coefficients

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    combined friction and heat transfer combined friction and area change conditions at sonic point transonicflow measurements in compressible flows.

    References:

    Shapiro, A. H., Dynamics and Thermodynamics of Compressible Fluid Flow, Vol. 1 & 2, Wiley & Sons(1953).

    1.

    Liepmann, H. W. and Roshko, A., Elements of Gas Dynamics, Dover Publications (2001).2.

    Thompson, P. A., Compressible Fluid Dynamics, McGraw-Hill (1972).3.

    Saad, M. A., Compressible Fluid Flow, 2

    nd

    ed., Prentice-Hall (1993).4.John, J. E. A. and Keith, T., Gas Dynamics, 3rd ed., Prentice-Hall (2006).5.

    Rathakrishnan, E., Gas Dynamics, 2nd ed., Prentice-Hall (2009).6.

    AE614 ADVANCED HEAT TRANSFER 4 credits

    Introduction review of heat transfer fundamentals transient conduction and extended surface heat transfer convection; hydrodynamically/ thermally devevloped and developing flows, influence of Prandtl number analogybetween momentum, heat, heat mass transfer steady laminar and turbulent heat transfer in external and internalflows heat transfer at high speeds unsteady laminar and turbulent forced convection in ducts and on plates convection with body forces two phase flow correlations radiation basics radiation in enclosures gasradiation diffusion and convective mass transfer combined heat and mass transfer from plates and in pipes.

    References:

    Incropera, F. P. and DeWitt, D. P., Fundamentals of Heat and Mass Transfer, 5th ed., John Wiley (2002).1.

    Kays, K. M. and Crawford, M. E., Convective Heat and Mass Transfer, 3rd ed., McGraw-Hill (1993).2.

    Bejan, A., Convective Heat Transfer, Wiley & Sons (1984).3.

    Edwards, D. K., Radiation Heat Transfer Notes, Hemisphere Wiley & Sons (1981).4.

    Arpaci, V. S., Conduction Heat Transfer, Abridged Edition, Ginn Press (1991).5.

    SEMESTER II

    AEXXX COMPUTATIONAL FLUID DYNAMICS 3 credits

    Mathematical models for fluid dynamics classification of partial differential equations discretization methods finite difference and finite volume formulations numerical solution of elliptic equations linear system ofalgebraic equations numerical solution of parabolic equations stability analysis numerical solution ofhyperbolic equations isentropic flow through CD nozzle simulation of shockwave formation incompressibleNavier-Stokes equations and their solution algorithms basics of grid generation.

    References:

    Hirsch, C., Numerical Computation of Internal and External Flows, Vol. I, 2nd ed., Butterworth-Heinemann(2007). Fisrt published by Wiley.

    1.

    Tannehill, J. C., Anderson, D. A., and Pletcher, R. H., Computational Fluid Mechanics and Heat Transfer,2nd ed., Taylor & Francis (1997).

    2.

    Hoffmann, K. A. and Chiang, S. T., Computational Fluid Dynamics for Engineers, 4th ed., EngineeringEducation Systems (2000).

    3.

    Anderson, J. D., Computational Fluid Dynamics: The Basics with Applications, McGraw-Hill (1995).4.

    Patankar, S. V., Numerical Heat Transfer and Fluid Flow, Hemisphere Pub. Corporation (1980).5.

    Ferziger, J. H. and Peric, M., Computational Methods for Fluid Dynamics, 3rd ed., Springer (2001).6.

    AEXXX MEASUREMENTS IN FLUID AND THERMAL SCIENCES 3 credits

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    Introduction configuration of an experimental set-up-error-calibration Uncertainity Analysis: error propagationformula, analysis of scatter, design of experiments based on uncertainty Review of probes and transducers:integral measurements of volume, velocity and temperature Introduction to wind tunnels: open and closed circuittunnels Optical instrumentation: lasers and coherent optics, refractive index variation in transparent media,interferometry, schlieren and shadowgraph methods, analysis of interferograms, Rayleigh scattering technique Transient response and instruments: zeroth, first and second order systems, treatment of spatially distributedvariables, compensation and recovery of original signals from measured data Computerized data acquisition.

    References:

    Holman, J. P., Experimental Methods for Engineers, 7th ed., Tata McGraw-Hill (2006).1.

    Doeblin, E. O., Measurement Systems-Application & Design 4th ed., McGraw-Hill (1998).2.

    Venkateshan, S. P., Mechanical Measurements, Ane Books, India (2008).3.

    Meshende, D., Optics, light and Lasers, (2004).4.

    AEXXX BOILING AND CONDENSATION 3 credits

    Pool Boiling: Nukiyama Experiment theory of vapor bubble formation mechanism of CHF various models andcorrelations.

    Flow boiling: homogeneous and heterogeneous models boiling enhancement techniques heat pipes.

    Condensation: film and dropwise condensation Nusselts analysis of laminar film condensation on vertical flatplate single horizontal tube and vertical array of tubes laminar-wavy and turbulent film condensation filmcondensation inside horizontal tubes, condensation enhancement techniques.

    References:

    Collier, J. G. and Thome, J. R., Convective Boiling and Condensation, 3rd ed., Oxford Univ. Press (2002).1.

    Lock, G. S. H., Latent Heat Transfer: An Introduction to Fundamentals, Oxford Univ. Press (1996).2.

    Tong, L. S. and Tang, Y. S., Boiling Heat Transfer and Two-Phase Flow, 2nd ed., Taylor & Francis (1997).3.

    Hewitt, G. F., Shires, G. L., and Bott, T. R., Process Heat Transfer, CRC Press (1994).4.

    AEXXX AEROSPACE PROPULSION 3 credits

    Introduction to Air-breathing and Rocket propulsion systems review of compressible flow with friction and heattransfer classification of air-breathing engines thrust and performance evaluation cycle analysis of ramjet,turbojet, turbofan, turboprop diffuser and nozzle component analysis combustion chambers ' rocketpropulsion systems classification performance parameters of rocket propulsion nozzle flow theory chemicalrockets liquid rocket engine cycles liquid propellants solid propellant rockets.

    References:

    Farokhi, S., Aircraft Propulsion, Wiley (2009).1.

    Sutton, G. P. and Biblarz, O., Rocket Propulsion Elements, 7th ed., Wiley (2001).2.

    Flack, R. D., Fundamentals of Jet Propulsion with Applications, Cambridge Univ. Press (2005).3.

    Hill, P. and Peterson, C., Mechanics and Thermodynamics of Propulsion 2nd

    ed., Prentice Hall (1991).4.Mattingly, J. D., Elements of Propulsion: Gas Turbines and Rockets, AIAA Edu. Series (2006).5.

    Mukunda, H. S., Understand Combustion, McMillan (1989).6.

    AEXXX TURBOMACHINES 3 credits

    Classification specific work representation of specific work in T-s and h-s diagrams Internal and externallosses Euler's equation of turbomachinery ideal and actual velocity triangles slip and its estimation impulseand reaction type machines degree of reaction effect of outlet blade angle on blade shape model laws,specific speed and shape number special features of steam and gas turbines performance characteristics ofturbomachines cavitation, surge and stall thin aerofoil theory cascade mechanics.

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    References:

    Dixon, S. L.,Fluid Mechanics, Thermodynamics of Turbomachinery, 4th ed., Butterworth-Heinemann(1998).

    1.

    Baskharone, E. A.,Principles of Turbomachinery and in Air-Breathing Engines, Cambridge University Press(2006).

    2.

    Wright, T.,Fluid Machinery: Performance, Analysis, and Design, CRC Press (1999).3.

    AEXXX SHOCKWAVE DYNAMICS 3 credits

    Hugoniot relation normal shocks unsteady 1-D flows finite amplitude waves characteristics Riemanninvariants unsteady shock waves shock tubes shock tunnels weak and strong shocks shock interactions reflections shock-boundary layer interaction shock polar diffraction shock focussing contactdiscontinuities Ritchmeyer-Meshcov instability spherical blast waves internal, near-field and externalballistics various shock structures.

    References:

    Glass, I. I. and Sislian, J. P., Nonstationary Flows And Shock Waves, Oxford Univ. Press (1994).1.

    Ben-Dor, G., Shock Wave Reflection Phenomena, Springer (2007).2.

    George, R., Nonsteady Duct Flow: Wave-diagram Analysis, Dover Publications (1969).3.

    Courant, R. and Friedrichs, K. O., Supersonic Flow and Shock Waves, Springer-Verlag (1976).4.

    AEXXX HYPERSONIC AIR-BREATHING PROPULSION 3 credits

    Hypersonic air-breathing propulsion overview of hypersonic propulsion research challenges in system design system performance and analysis hypersonic intakes supersonic combustors expansion systems enginecooling liquid air-cycle engines space plane applications experimental and testing facilities CFDapplications and simulation excercises.

    References:

    Heiser, W. H. and Pratt, D. T., Hypersonic Air-breathing Propulsion, AIAA Edu. Series (1994).1.

    Curran, E. T. and Murthy, S. N. B., (Eds.) Scramjet Propulsion, AIAA Edu. Series (2001).2.

    Segal, C., The Scramjet Engine Processes and Characteristics, Cambridge Univ. Press (2011).3.

    AEXXX MICROSCALE AND NANOSCALE HEAT TRANSFER 3 credits

    Microscale heat transfer electronics cooling and MEMS applications convective heat transfer in microtubes andchannels boiling and two-phase flow mathematical modeling nanoscale heat transfer phenomena conduction, convection, and radiation in the nanoscale applications simulation methods multicarrier andmultidimensional transport.

    References:

    Kandlikar, S., Garimella, S., Li, D., Colin, S., and King, M. R., Heat Transfer and Fluid Flow in Minichannels

    and Microchannels, Elsevier (2005).

    1.

    S. Kakac, Vasiliev, L. L., Bayazitoglu, Y., and Yener, Y., Microscale Heat Transfer Fundamentals andApplications, Springer (2004).

    2.

    Sobhan, C. B. and Peterson, G. P., Microscale and Nanoscale Heat Transfer: Fundamentals andEngineering Applications, CRC Press (2008).

    3.

    AEXXX CRYOGENIC ENGINEERING 3 credits

    Cryogenic Engineering: Historical background and applications gas liquefaction systems gas separation andgas purification systems cryogenic refrigeration systems storage and handling of cryogens cryogenicinsulations liquefied natural gas-properties of materials of low temperatures material of construction and

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    techniques of fabrication instrumentation ultra-low temperature techniques application.

    References:

    Barron, R. F., Cryogenic Systems, 2nd ed., Oxford Univ. Press (1985).1.

    Weisend, J. G., The Handbook of Cryogenic Engineering, Taylor & Francis (1998).2.