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Friday, December 28, 2012

AE2024 HEAT TRANSFER SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 6TH SEMESTER SYLLABUS REGULATION 2008 2011 2012-2013

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AE2024 HEAT TRANSFER SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 6TH SEMESTER SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY SIXTH SEMESTER B.E AERONAUTICAL ENGINEERING DEPARTMENT SYLLABUS, TEXTBOOKS, REFERENCE BOOKS,EXAM PORTIONS,QUESTION BANK,PREVIOUS YEAR QUESTION PAPERS,MODEL QUESTION PAPERS, CLASS NOTES, IMPORTANT 2 MARKS, 8 MARKS, 16 MARKS TOPICS. IT IS APPLICABLE FOR ALL STUDENTS ADMITTED IN THE YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI, TIRUNELVELI,COIMBATORE), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009

AE2024 HEAT TRANSFER L T P C
3 0 0 3
OBJECTIVE
To introduce the concepts of heat transfer to enable the students to design components
subjected to thermal loading.
UNIT I HEAT CONDUCTION 11
Basic Modes of Heat Transfer – One dimensional steady state heat conduction:
Composite Medium – Critical thickness – Effect of variation of thermal Conductivity –
Extended Surfaces – Unsteady state.
Heat Conduction: Lumped System Analysis – Heat Transfer in Semi infinite and infinite
solids – Use of Transient – Temperature charts – Application of numerical techniques.
73
UNIT II CONVECTIVE HEAT TRANSFER 10
Introduction – Free convection in atmosphere free convection on a vertical flat plate –
Empirical relation in free convection – Forced convection – Laminar and turbulent
convective heat transfer analysis in flows between parallel plates, over a flat plate and in a
circular pipe. Empirical relations, application of numerical techniques in problem solving.
UNIT III RADIATIVE HEAT TRANSFER 8
Introduction to Physical mechanism – Radiation properties – Radiation shape factors –
Heat exchange between non – black bodies – Radiation shields.
UNIT IV HEAT EXCHANGERS 8
Classification – Temperature Distribution – Overall heat transfer coefficient, Heat
Exchange Analysis – LMTD Method and E-NTU Method.
UNIT V HEAT TRANSFER PROBLEMS IN AEROSPACE ENGINEERING 8
High-Speed flow Heat Transfer, Heat Transfer problems in gas turbine combustion
chambers – Rocket thrust chambers – Aerodynamic heating – Ablative heat transfer.
TOTAL: 45 PERIODS
TEXT BOOKS
1. Yunus A. Cengel., “Heat Transfer – A practical approach”, Second Edition, Tata
McGraw-Hill, 2002.
2. Incropera. F.P.and Dewitt.D.P. “ Introduction to Heat Transfer”, John Wiley and Sons
– 2002.
REFERENCES
1. Lienhard, J.H., “A Heat Transfer Text Book”, Prentice Hall Inc., 1981.
2. Holman, J.P. “Heat Transfer”, McGraw-Hill Book Co., Inc., New York, 6th Edn., 1991.
3. Sachdeva, S.C., “Fundamentals of Engineering Heat & Mass Transfer”, Wiley Eastern
Ltd., New Delhi, 1981.
4. Mathur, M. and Sharma, R.P. “Gas Turbine and Jet and Rocket Propulsion”, Standard
Publishers, New Delhi 1988.

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