{"id":58809,"date":"2023-09-05T13:14:04","date_gmt":"2023-09-05T13:14:04","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/as3003-launch-vehicle-aerodynamics-syllabus-for-aerospace-engg-2021-regulation-professional-elective-i\/"},"modified":"2023-09-05T13:14:04","modified_gmt":"2023-09-05T13:14:04","slug":"as3003-launch-vehicle-aerodynamics-syllabus-for-aerospace-engg-2021-regulation-professional-elective-i","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/as3003-launch-vehicle-aerodynamics-syllabus-for-aerospace-engg-2021-regulation-professional-elective-i\/","title":{"rendered":"AS3003: Launch Vehicle Aerodynamics syllabus for Aerospace Engg 2021 regulation (Professional Elective-I)"},"content":{"rendered":"

Launch Vehicle Aerodynamics detailed syllabus for Aerospace Engineering (Aerospace Engg) for 2021 regulation curriculum has been taken from the Anna Universities<\/a> official website and presented for the Aerospace Engg students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below. <\/p>\n

For Aerospace Engineering 5th Sem scheme and its subjects, do visit Aerospace Engg 5th Sem 2021 regulation scheme<\/a>. For Professional Elective-I scheme and its subjects refer to Aerospace Engg Professional Elective-I syllabus scheme<\/a>. The detailed syllabus of launch vehicle aerodynamics is as follows. <\/p>\n

Course Objectives:<\/h4>\n

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Unit I<\/h4>\n

BASICS OF HIGH-SPEED AERODYNAMICS
\nCompressible flows-Isentropic relations-mathematical relations of flow properties across shock and expansion waves-fundamentals of Hypersonic Aerodynamics.\n<\/p>\n

Unit II<\/h4>\n

BOUNDARY LAYER EFFECTS
\nBasics of boundary layer theory-compressible boundary layer-shock shear layer interaction-Aerodynamic heating-heat transfer effects on launch vehicle.\n<\/p>\n

Unit III<\/h4>\n

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Unit IV<\/h4>\n

AERODYNAMICS OF SLENDER AND BLUNT BODIES
\nAerodynamics of slender and blunt bodies, (flwing-body interference effects-Asymmetric flow separation and vortex shedding-unsteady flow characteristics of launch vehicles- determination of aero elastic effects.\n<\/p>\n

Unit V<\/h4>\n

AERODYNAMIC ASPECTS OF LAUNCHING PHASE
\nBooster separation-cross wind effects-specific considerations in missile launching -missile integration and separation-methods of evaluation and determination- Stability and Control Characteristics of Launch Vehicle Configuration- Wind tunnel tests – Comparison with CFD Analysis.\n<\/p>\n

Course Outcomes:<\/h4>\n

On successful completion of this course, the student will be able to<\/p>\n