Study Programmes 2015-2016
AERO0033-1  
Aerothermodynamics of high-speed flows
Duration :
30h Th, 30h Pr, 1d FW
Number of credits :
Master in aerospace engineering (120 ECTS)5
Master in aerospace engineering (120 ECTS)5
Lecturer :
Thierry Magin
Language(s) of instruction :
English language
Organisation and examination :
Teaching in the second semester
Units courses prerequisite and corequisite :
Prerequisite or corequisite units are presented within each program
Course contents :
This course introduces students to the aerothermodynamic analysis of high speed flows. Two main subjects are addressed: - Transonic and supersonic aerodynamics - Atmospheric reentry and plasma physics
Learning outcomes of the course :
The aim of this course is to introduce students to some aspects of high speed aerothermodynamics.
The detailed objectives are:
- Introduction to transonic and supersonic flows - Calculation of lift and drag of 2D wings at transonic and supersonic conditions - Calculation of lift and drag of 3D wings and aircraft at transonic and supersonic conditions - Application of the characteristic method to one-dimensional unsteady flows - Introduction to chemically reacting and plasma flows encountered in hypersonic and combustion applications - Solutions to some practical problems encountered in aerospace missions, focusing on the simulation of atmospheric entry flows and ground testing
Prerequisite knowledge and skills :
AERO0001-1 Aerodynamics MECA0025-1 Fluid mechanics
Planned learning activities and teaching methods :
This is a second semester course. It is divided into lectures and practical sessions.
Students are familiarized with high enthalpy facilities during a laboratory session. Teaching assistants operate a wind-tunnel during a lab demonstration at the von Karman Institute for Fluid Dynamics.
Mode of delivery (face-to-face ; distance-learning) :
Face-to-face in English
Recommended or required readings :
The lecture notes are available online in the form of presentations.
Supplementary textbooks: J. Anderson, Modern Compressible Flow: With Historical Perspective, McGraw-Hill, 2002 J. D. Anderson, Hypersonic and high-temperature gas dynamics, American Institute of Aeronautics and Astronautics, 2006 P. A. Thompson, Compressible-fluid Dynamics, Advanced engineering series, 1988
Assessment methods and criteria :
Assessment is performed through: - A written exam - A homework assignment following the laboratory session
Work placement(s) :
N/A
Organizational remarks :
Contacts :
Prof. G. Dimitriadis Aeroelasticity and Experimental Aerodynamics (AEA) Department of Aerospace and Mechanical Engineering  1 Chemin des Chevreuils (B52/3) Room +2/424  Tel: +32 (0)4 3669815 Email: gdimitriadis@ulg.ac.be


Prof. T. Magin Aeronautics and Aerospace Department von Karman Institute for Fluid Dynamics Chaussee de Waterloo 72 1640 Rhode-Saint-Genese Tel: +32 (0)2 359 96 38 Email:  magin@vki.ac.be