31th Congress of the International Council of the Aeronautical Sciences

03.1 - Aerodynamics - CFD Methods and Validation

ANALYSIS OF CHEMICALLY REACTING HYPERSONIC FLOW USING A MESHLESS METHOD

D. Hanı, J.Y. Huhı, S. Nohı, K.H. Kimı; ıSeoul National University, South Korea

This study aims to develop a computational aerothermal solver which is capable of calculating hypersonic flow and structural thermal response. Governing equations for non-equilibrium flow which consists of 5 chemical species and structural thermal response are discretized using a meshless method.


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