Compressible Aerodynamics

课程简介

/ Indicative Syllabus Linearised Flow – Full Velocity Potential Equation; Linearised Subsonic Flow; Compressibility Corrections; Linearised Supersonic Flow. Transonic Flows –Velocity Potential Equations for Sub-transonic and Super- transonic Flows; Prandtl-Glauert Rule; Critical Mach number; Drag Divergence; Supercritical Airfoil; Swept Wings; Area Rule. One-Dimensional – Normal Shock Relations; One-Dimensional Flow with Heat Addition; One-Dimensional Flow with Friction; Quasi-One-Dimensional Flows –Area-Velocity Relation; Convergent/Divergent Nozzles and Diffusers. Oblique Shock and Expansion Waves – Oblique Shock Relations; Shock Polar; Pressure-Deflection Diagrams; Shock Interactions; Conical Flow; Prandtl-Meyer Expansion Waves; Supersonic Airfoils. Unsteady Supersonic Flows – Shock Tube Equations; Detonation -- 1 of 3 --

目标

1. To provide students with knowledge in compressible aerodynamics; and 2. To develop students’ capability in aerodynamic analysis of canonical geometries, nozzles, airfoils and wings with the consideration of compressibility.

先修要求

/ Co-requisite/ Exclusion Nil

Teaching Pattern

Methodology 1. The teaching and learning methods include lectures/tutorial sessions, homework assignments, test and examination. 2. The continuous