Advanced Aerodynamics

课程简介

/ Indicative Syllabus One-Dimensional and Quasi-One-Dimensional Flows – Normal Shock Relations; One-Dimensional Flow with Heat Addition; One-Dimensional Flow with Friction; Area-Velocity Relation; Nozzles and Diffusers. Oblique Shock and Expansion Waves – Oblique Shock Relations; Shock Polar; Pressure-Deflection Diagrams; Shock Interactions; Conical Flow; Prandtl-Meyer Expansion Waves. Linearized Flow – Velocity Potential Equation; Linearized Subsonic Flow; Compressibility Corrections; Linearized Supersonic Flow. Transonic and Hypersonic Flows – Full Velocity Potential Equation; Newtonian Theory; Mach Number Independence; Hypersonic Small- Disturbance Equations; Statistical Thermodynamics; Kinetic Theory; High- Temperature Gas Dynamics. Boundary-Layer Flow – Boundary-Layer Equations; Self-Similar Solutions; Von Kármán Momentum Integral; Boundary-Layer Transition; Linear Stability Theory; Turbulent Boundary Layer; Turbulence Modeling; Hypersonic Viscous Interactions; Shock-Wave/Boundary-Layer Interactions. -- 1 of 3 --

目标

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

先修要求

/ Co-requisite/ Exclusion N/A

Teaching Pattern

Methodology 1. The teaching and learning methods include lectures/tutorial sessions, homework assignments and case study report and presentation. 2. Technical/scientific examples and problems are raised and discussed in class/tutorial sessions. 3. Case study report and presentation will be applied to provide students a guided study with the basic research elements, including literature review, research methodology, experimental/numerical data analysis and presentation skill. Teaching/Learning Methodology Intended subject learning outcomes a b c d 1. Lecture √ √ √ √ 2. Tutorial √ √ √ 3. Homework assignment √ √ √ 4. Case study report and presentation √ √ √ √