AVBa - AVBP Airfoil Computation

Author : Frédéric Ducros, CERFACS - ducros@cerfacs.fr
Objectives :
This project centers around 2D airfoil calculations. The computations are based on the unstructured flower solver AVBP of CERFACS. For two differents meshes and flow regimes the three following tasks are proposed:
Working plan :

Week

1

2

3

4

5

6

AVBa.1 

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*

 

 

 

 

AVBa.2 

 

***

**

 

 

 

AVBa.3 

 

 

**

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AVBa.4 

 

 

 

 

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Exam

 

 

 

 

 

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Deliverables :
1. Velocity and pressure fields around the airfoils.
2. Polars and angles of limit stall.
3. Convergence history as function of incidence and artificial diffusion.
Bibliography :
[1] The AVBP User's Manual, T. Schönfeld, CERFACS, 1999.
[2] Cours de FORTRAN77/90.
Pedagogical interest :
Introduction to some basic aeronautical CFD problems.


 

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