Computational tools for supporting the testing of civil aircraft configurations in wind tunnels

Author:

Bosnyakov S.,Kursakov I.,Lysenkov A.,Matyash S.,Mikhailov S.,Vlasenko V.,Quest J.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference65 articles.

1. Bosniakov SM. Approach to real aircraft 3D calculation based on time-dependent Euler equation system with boundary layer taking into account. Research Bulletin no. 6, Warsaw University of Technology, 1997.

2. Bosniakov S, Glazkov S, Matyash S, Neyland V, Remeev N, Yatckevich N. Numerical modelling flow-field around model in the big transonic wind tunnel using monotone 2nd order Godunov-type scheme. In: Wind tunnels and wind tunnel test techniques, Proceedings, Cambridge, UK, April 1997. p. 14–6.

3. Experience in integrating CFD to the technology of testing models in wind tunnels;Bosniakov;Progr Aerospace Sci,1998

4. Conception of electronic wind tunnel and first results of its implementation;Neyland;Progr Aerospace Sci,2001

5. A perspective on computational algorithms for aerodynamic analysis and design;Jameson;Progr Aerospace Sci,2001

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