Astraios Courses3251
hasCourse

Computational aerodynamics  

Description

This module aims to develop a basic understanding of the aerodynamic behaviour for both 2D and 3D wings. Students will be required to demonstrate knowledge from Fluid Mechanics leading up to Kutta-Joukowski Theorem. Students then apply General Thin Airfoil theory to develop 2D wing flow characteristics and Prandtl’s lifting line theory to derive Aerodynamic coefficients for 3D finite wings. Students will also be required to apply knowledge through computational methods to demonstrate the derived theory and analyse the aerodynamics of a UAV wing.

Delivery mode

Presential
English

Name

Computational aerodynamics
English

UNIVERSITY OF TWENTE

Faculty of Geo-Information Science and Earth Observation

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