Article

Numerical simulation of a flow around airfoil using inviscid gas equations

Russian Aeronautics (Iz VUZ) 04/2012; 52(1):114-119. DOI:10.3103/S1068799809010206 pp.114-119

ABSTRACT A method for determining a field of inviscid gas equation application in finding the aerodynamic characteristics of bodies
is proposed; as an example, use is made of airfoils for which extensive experimental data are available. The comparative analysis
of physical and numerical simulation results showed a good verification of the method presented.

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Keywords

aerodynamic characteristics
 
comparative analysis
 
extensive experimental data
 
inviscid gas equation application
 
numerical simulation results