Anna University Syllabus - Anna University ME Syllabus
AS7202 LAUNCH VEHICLE AERODYNAMICS Syllabus | Anna University ME Aerospace Technology (LVT) Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aerospace Technology(Launch Vehicle Technology), 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 Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.
Anna University Chennai Syllabus
AS7202 LAUNCH VEHICLE AERODYNAMICS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, Students will learn the concept of high speed aerodynamics and
configurations of launch vehicles.
UNIT I BASICS OF HIGH SPEED AERODYNAMICS 9
Compressible flows-Isentropic relations-mathematical relations of flow properties across shock and
expansion waves-fundamentals of Hypersonic Aerodynamics
UNIT II BOUNDARY LAYER THEORY 9
Basics of boundary layer theory-compressible boundary layer-shock shear layer interaction-
Aerodynamic heating-heat transfer effects
UNIT III LAUNCH VEHICLE CONFIGURATIONS AND DRAG ESTIMATION 9
Types of Rockets and missiles-various configurations-components-forces on the vehicle during
atmospheric flight-nose cone design and drag estimation
UNIT IV AERODYNAMICS OF SLENDER AND BLUNT BODIES 9
Aerodynamics of slender and blunt bodies, wing-body interference effects-Asymmetric flow separation
and vortex shedding-unsteady flow characteristics of launch vehicles- determination of aero elastic
effects.
UNIT V AERODYNAMIC ASPECTS OF LAUNCHING PHASE 9
Booster 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.
L : 45, TOTAL: 45 PERIODS
REFERENCES:
1. Anderson, J.D., “Fundamentals of Aerodynamics”, McGraw-Hill Book Co., New York, 1985.
2. Chin SS, Missile Configuration Design, Mc Graw Hill, New York, 1961.
3. Anderson, J.D., “Hypersonic and High Temperature Gas Dynamics”, AIAA Education Series.
4. Nielson, Jack N, Stever, Gutford, “Missile Aerodynamics”, Mc Graw Hill, New York, 1960.
5. Anderson Jr., D., – “Modern compressible flows”, McGraw-Hill Book Co., New York 1999.
6. Charles D.Brown, “Spacecraft Mission Design”, AIAA Education Series, Published by AIAA, 1998
7. Elements of Space Technology for Aerospace Engineers”, Meyer Rudolph X, Academic Press,
1999
AS7202 LAUNCH VEHICLE AERODYNAMICS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, Students will learn the concept of high speed aerodynamics and
configurations of launch vehicles.
UNIT I BASICS OF HIGH SPEED AERODYNAMICS 9
Compressible flows-Isentropic relations-mathematical relations of flow properties across shock and
expansion waves-fundamentals of Hypersonic Aerodynamics
UNIT II BOUNDARY LAYER THEORY 9
Basics of boundary layer theory-compressible boundary layer-shock shear layer interaction-
Aerodynamic heating-heat transfer effects
UNIT III LAUNCH VEHICLE CONFIGURATIONS AND DRAG ESTIMATION 9
Types of Rockets and missiles-various configurations-components-forces on the vehicle during
atmospheric flight-nose cone design and drag estimation
UNIT IV AERODYNAMICS OF SLENDER AND BLUNT BODIES 9
Aerodynamics of slender and blunt bodies, wing-body interference effects-Asymmetric flow separation
and vortex shedding-unsteady flow characteristics of launch vehicles- determination of aero elastic
effects.
UNIT V AERODYNAMIC ASPECTS OF LAUNCHING PHASE 9
Booster 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.
L : 45, TOTAL: 45 PERIODS
REFERENCES:
1. Anderson, J.D., “Fundamentals of Aerodynamics”, McGraw-Hill Book Co., New York, 1985.
2. Chin SS, Missile Configuration Design, Mc Graw Hill, New York, 1961.
3. Anderson, J.D., “Hypersonic and High Temperature Gas Dynamics”, AIAA Education Series.
4. Nielson, Jack N, Stever, Gutford, “Missile Aerodynamics”, Mc Graw Hill, New York, 1960.
5. Anderson Jr., D., – “Modern compressible flows”, McGraw-Hill Book Co., New York 1999.
6. Charles D.Brown, “Spacecraft Mission Design”, AIAA Education Series, Published by AIAA, 1998
7. Elements of Space Technology for Aerospace Engineers”, Meyer Rudolph X, Academic Press,
1999
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