Числовий аналіз

The development of computational fluid dynamics and heat transfer software for supersonic flow interactions

Лінії плівкової течії по твердій стінці в порівнянні з лініями поверхневої течії крапель у експерименті (конфігурація корпус – газовий струмінь)

Gas-dynamic and heat transfer mathematical model of supersonic flow over flying vehicles is developed. The model is taken into account with medium compressibility and dissipative effects leading to an increase of heating rate. Proposed model is based on physical interaction of shock wave and boundary layer. Three dimensional numerical models of flying vehicles in gas-dynamic states are developed in order to investigate different configurations concerning such systems as case - sharp swept fin, case - perpendicular cylinder, case - gas jet, case - sharp unswept fin.