JNTUK B.Tech Hypersonic Aerodynamics gives you detail information of Hypersonic Aerodynamics R13 syllabus It will be help full to understand you complete curriculum of the year.
Course Objectives
Develop an understanding of inviscid hypersonic flows, viscous hypersonic flows and high temperature effects as they apply to hypersonic aerodynamics.
UNIT-I – Fundamentals Of Hypersonic Flows: Importance/properties of hypersonic flow-Basic equations boundary conditions for inviscid flow, shock wave shapes, flow over a wedge
UNIT-II – Hypersonic Approximations: Prandtl-Meyer flow- Axi-symmetric flow over a cone – Flow over a flat plate.
Hypersonic Small Disturbance Theory: Flow over a wedge and a cone- Blast wave analogy,-Newtonian impact theory- Busemann centrifugal correction – Shock expansion method- Tangent cone and tangent wedge methods
UNIT-III – Basic Aspects Of Hypersonic Viscous Flows: Introduction to viscous flow and pressure interactions over flat plate- Boundary layers
Hypersonic Viscous Interactions: Strong and weak interactions-Shock wave/ boundary layer interactions
UNIT-IV – Hypersonic Aerodynamic Heating: Reference temperature method-Entropy layer effects on aerodynamic heating.
UNIT-V – Hypersonic Vehicle Design: Hypersonic propulsion and vehicle design
UNIT-VI- Rarefied Gas Dynamics: Rarefied flow regimes-Kinetic theory of gases-Gas-surface interaction- Aerodynamic forces in hypersonic free molecular flow around simple geometries
TEXT BOOKS
- “Hypersonic and High Temperature Gas Dynamics”, Anderson, J.D,McGraw-Hill, 1989.
- “Hypersonic Aerothermodynamics”, Bertin, J.J., AIAA, 1994.
REFERENCE BOOKS
- “Introduction to Hypersonic flow”, Cherni C G, Academic Press,1961
- “Hypersonic Flow Theory”, Hayes W D and Problein R F, Academic Press 1959
- “Elements of Hypersonic Aerodynamics”, Cox R N and Crabtree L P, London 1965
Course Outcomes
Students who successfully complete the course will demonstrate the following outcomes
- An ability to solve problems involving inviscid hypersonic flows
- An ability to solve problems involving viscous hypersonic flows.
- An understanding of high temperature effects in hypersonic aerodynamics.
- An understanding of the design issues for hypersonic wings.
- An ability to use computational tools to evaluate hypersonic flows.
- Knowledge of recent developments in hypersonic aerodynamics with application to aerospace systems.
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