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Laboratory Simulation of Supersonic Air Flow Paternsдоклад на конференции
- Авторы: Kotov M.A., Ruleva L.B., Solodovnikov S.I., Surzhikov
- Международная Конференция : Proceedings of international conference “Fluexes and structures in fluids”
- Даты проведения конференции: 8-14 августа 2018
- Дата доклада: 9 августа 2018
- Тип доклада: Стендовый
- Докладчик: не указан
- Место проведения: Владивостолк, Russia
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Аннотация доклада:
Successful flights of advanced high-speed aircraft at altitudes of 30 ... 60 km above the ground were preceded by computational and experimental studies of their models with simu-lation of the working environment and operating conditions. National calculation codes [1-3] describing aerothermodynamics of perspective aircrafts have been developed and are being developed in the Ishlinsky Institute for Problems in Mechanics RAS (IPMech RAS). Author computer code results are validating by means of the HAST experimental setup (Hypersonic Aerodynamic Shock Tube) at the Institute.
- Добавил в систему: Рулева Лариса Борисовна