The article presents the results of calculating the aerodynamic characteristics for a super-sonic gas flow around the AGARD-B vehicle model at Mach numbers 4 and 5.1 in the range of angles-of-attack 4o÷ 9.19o.
Результаты расчетов сверхзвукового течения газа около модели аппарата AGARD-B
Приведены результаты расчета аэродинамических характеристик при обтекании сверхзвуковым потоком газа модели аппарата AGARD-В при числах Маха 4 и 5.1 в диапазоне углов атаки от − 4о до 9.19о.
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