Numerical modeling of aerodynamic wind tunnel experiment

Authors: Marashan М.V.
Published in issue: #5(5)/2016
DOI: 10.18698/2541-8009-2016-5-46
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control
Keywords: aerodynamic experiment, wind tunnel, numerical simulation, Solid Works Flow Simulation
Published: 14.03.2017

We developed a model of the wind tunnel test section for aerodynamic numerical simulation experiment in the tunnel T-500, developed in Bauman Moscow State Technical University. We carried out numerical modeling of the experiment according to the example of the profile blasting V simm. - 12 %. We drew the comparison between the results of profile blastng V simm. - 12 % in the wind tunnel T-500 test section and the results of blasting in the tunnel T-102, developed in Central Aerohydrodynamic Institute as a result of numerical simulation. We obtained close agreement of results of numerical modeling and experimental data presented in the works of Central Aerohydrodynamic Institute.

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