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.<\/p>\n
The detailed syllabus for Aerodynamics – II B.Tech (R13) fifthsem is as follows<\/p>\n
OBJECTIVES<\/strong>:<\/p>\n UNIT I : FUNDAMENTAL ASPECTS OF COMPRESSIBLE FLOW<\/strong> \u00a0 \u00a0[9 hours] UNIT II: SHOCK AND EXPANSION WAVES<\/strong> \u00a0 \u00a0\u00a0[10 hours] UNIT III : TWO DIMENSIONAL COMPRESSIBLE FLOW<\/strong> \u00a0 \u00a0 \u00a0[9 hours]\n
\nCompressibility, continuity, momentum and energy equations for steady one dimensional flow,\u00a0compressible bernoulli\u2019s equation, area \u2013 mach number \u2013 velocity relation, mach cone, mach angle,\u00a0one dimensional isentropic flow through variable area duct, critical conditions, characteristic mach\u00a0number, area-mach number relation, maximum discharge velocity \u2013 operating characteristics of\u00a0nozzles- introduction to hypersonic flows<\/p>\n
\nNormal shock relations, Prandtl\u2019s relation, Hugoniot equation, Rayleigh Supersonic Pitot tube\u00a0equation, Moving normal shock waves, Oblique shocks, \u00a0M relation, Shock Polar, Reflection of\u00a0oblique shocks, left running and right running waves, Interaction of oblique shock waves, slip line,\u00a0shock-boundary layer interaction \u2013 transonic lambda shock \u2013 compression corner effect \u2013 incident\u00a0shock interaction – Rayleigh flow, Fanno flow, Expansion waves, Prandtl Meyer expansion, Maximum\u00a0turning angle, Simple and non-simple regions.<\/p>\n
\nPotential equation for 2-dimensional compressible flow, Linearisation of potential equation,\u00a0perturbation potential, Linearised Pressure Coefficient, Linearised subsonic flow, Prandtl-Glauert rule,\u00a0Linearised supersonic flow, Method of characteristics.<\/p>\n