Aerodynamics – II Syllabus for B.Tech 5th sem is covered here. This gives the details about credits, number of hours and other details along with reference books for the course.
The detailed syllabus for Aerodynamics – II B.Tech (R13) fifthsem is as follows
OBJECTIVES:
- To introduce the concepts of compressibility,
- To make the student understand the theory behind the formation of shocks and expansion fans in Supersonic flows.
- To introduce the methodology of measurements in Supersonic flows.
UNIT I : FUNDAMENTAL ASPECTS OF COMPRESSIBLE FLOW [9 hours]
Compressibility, continuity, momentum and energy equations for steady one dimensional flow, compressible bernoulli’s equation, area – mach number – velocity relation, mach cone, mach angle, one dimensional isentropic flow through variable area duct, critical conditions, characteristic mach number, area-mach number relation, maximum discharge velocity – operating characteristics of nozzles- introduction to hypersonic flows
UNIT II: SHOCK AND EXPANSION WAVES [10 hours]
Normal shock relations, Prandtl’s relation, Hugoniot equation, Rayleigh Supersonic Pitot tube equation, Moving normal shock waves, Oblique shocks, M relation, Shock Polar, Reflection of oblique shocks, left running and right running waves, Interaction of oblique shock waves, slip line, shock-boundary layer interaction – transonic lambda shock – compression corner effect – incident shock interaction – Rayleigh flow, Fanno flow, Expansion waves, Prandtl Meyer expansion, Maximum turning angle, Simple and non-simple regions.
UNIT III : TWO DIMENSIONAL COMPRESSIBLE FLOW [9 hours]
Potential equation for 2-dimensional compressible flow, Linearisation of potential equation, perturbation potential, Linearised Pressure Coefficient, Linearised subsonic flow, Prandtl-Glauert rule, Linearised supersonic flow, Method of characteristics.
[TOTAL (L:45+T:15): 60 PERIODS]
OUTCOMES
- Understanding characterstics of fluid dlows
- Knowledge gained in shock phenomenon and fluid waves.
- understanding fluid flow characteristics over wings airfoils and airplanes.
- Usage of wind tunnels for evaluating flow behaviours.
TEXT BOOKS:
- Anderson, J. D, “Modern Compressible Flow”, McGraw-Hill & Co., 2002.
- Rathakrishnan., E,”Gas Dynamics”, Prentice Hall of India, 2004.
REFERENCES:
- Shapiro, A. H., “Dynamics and Thermodynamics of Compressible Fluid Flow”, Ronald Press, 1982.
- Zucrow, M. J. and Anderson, J. D., “Elements of Gas Dynamics”, McGraw- Hill & Co., 1989.
- Oosthuizen,P.H., & Carscallen,W.E., “Compressible Fluid Flow”, McGraw- Hill & Co.,1997
For all other B.Tech AE 5th sem syllabus go to Anna University B.Tech AERONAUTICAL ENGINEERING (AE) 5th Sem Course Structure for (R13) Batch.All details and yearly new syllabus will be updated here time to time.Subscribe, like us on facebook and follow us on google plus for all updates.
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