FUNDED CURRICULAM
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Global Academy of Technology, Bangalore
ANSYS Funded Curriculum Program – Feb 2024
Course: COMPRESSIBLE FLOW
Course Learning Objective:
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.
Course Description:
Module 1
1-D Compressible flow
Introduction to Compressible Flows, Flow Regimes, speed of Sound, Adiabatic Steady State Flow Equations, Flow-through Nozzle, diffuser and Convergent- Divergent Passage.
Module 2
Normal Shock Waves
Alternative form of Energy Equation, Rankine - Hugonoit Relation, Normal Shock relations, Rayleigh and Fanno Flow.
Module 3
Oblique Shock Wave Expansion waves
Oblique Shocks and Equations, Flow past over wedges, Concave and Convex corners. Strong & weak Shocks, Attached & Detached Shocks. Reflection, and Interaction of Shocks, Expansion waves.
Module 4
Linearized Flow
Velocity potential equation, Small Perturbation Theory & linearized subsonic & supersonic pressure co-efficient, Mach waves and Mach angles, Prandtl-Glauert compressibility correction.
Module 5
Transonic Flow over Wing
Lower and upper Critical Mach numbers, Lift and drag divergence Mach number, Shock induced separation, Characteristics of Swept wings, Transonic Area rule.
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