Gas dynamic effect of microwave discharge on supersonic cone-shaped bodies

V. A. Lashkov, I. Ch Mashek, Yu I. Anisimov, V. I. Ivanov, Yu F. Kolesnichenko, M. I. Ryvkin, A. A. Gorynya

Результат исследований: Материалы конференцийматериалы

19 Цитирования (Scopus)

Выдержка

The detailed experimental investigations are implemented for better understanding of phenomena taking place under interaction of MW discharge in supersonic flow with aerodynamic bodies. The set of measures is undertaken for raising of precision and reliability of the obtained results: Modernization of the wind tunnel, improvement of existing and application of new diagnostic equipment. New digital Schlieren system is constructed. which allows obtaining single-shot images of bodies streamlining with time exposure about 0.5μs, synchronized with a certain phase of a process under investigation. The measuring channel, which registers the weak discharge afterglow, let us observe evolution of an excited gas region under its interaction with investigated body. Measurements of pressure on the body surface are also performed. Blunt cylinder, hemisphere and cone are tested as experimental bodies. Investigation of aerodynamic effect of plasma interaction with bodies over their dimension is fulfilled. The mutual position of MW discharge region and AD body is shown as having a substantial importance. Experimental evidence of vortex origination in a shock layer while its interaction with heated region of discharge is presented, this vortex being the basic reason for body drag reduction.

Язык оригиналаанглийский
Страницы1551-1559
Число страниц9
СостояниеОпубликовано - 1 июл 2004
Событие42nd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, Соединенные Штаты Америки
Продолжительность: 5 янв 20048 янв 2004

Конференция

Конференция42nd AIAA Aerospace Sciences Meeting and Exhibit
СтранаСоединенные Штаты Америки
ГородReno, NV
Период5/01/048/01/04

Отпечаток

Gas dynamics
Discharge (fluid mechanics)
Cones
Aerodynamics
Vortex flow
Schlieren systems
Microwaves
Plasma interactions
Drag reduction
Supersonic flow
Modernization
Wind tunnels
Gases

Предметные области Scopus

  • Технология (все)

Цитировать

Lashkov, V. A., Mashek, I. C., Anisimov, Y. I., Ivanov, V. I., Kolesnichenko, Y. F., Ryvkin, M. I., & Gorynya, A. A. (2004). Gas dynamic effect of microwave discharge on supersonic cone-shaped bodies. 1551-1559. Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.
Lashkov, V. A. ; Mashek, I. Ch ; Anisimov, Yu I. ; Ivanov, V. I. ; Kolesnichenko, Yu F. ; Ryvkin, M. I. ; Gorynya, A. A. / Gas dynamic effect of microwave discharge on supersonic cone-shaped bodies. Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.9 стр.
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Lashkov, VA, Mashek, IC, Anisimov, YI, Ivanov, VI, Kolesnichenko, YF, Ryvkin, MI & Gorynya, AA 2004, 'Gas dynamic effect of microwave discharge on supersonic cone-shaped bodies' Документ представлен на, Reno, NV, Соединенные Штаты Америки, 5/01/04 - 8/01/04, стр. 1551-1559.

Gas dynamic effect of microwave discharge on supersonic cone-shaped bodies. / Lashkov, V. A.; Mashek, I. Ch; Anisimov, Yu I.; Ivanov, V. I.; Kolesnichenko, Yu F.; Ryvkin, M. I.; Gorynya, A. A.

2004. 1551-1559 Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.

Результат исследований: Материалы конференцийматериалы

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AU - Lashkov, V. A.

AU - Mashek, I. Ch

AU - Anisimov, Yu I.

AU - Ivanov, V. I.

AU - Kolesnichenko, Yu F.

AU - Ryvkin, M. I.

AU - Gorynya, A. A.

PY - 2004/7/1

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Lashkov VA, Mashek IC, Anisimov YI, Ivanov VI, Kolesnichenko YF, Ryvkin MI и соавт.. Gas dynamic effect of microwave discharge on supersonic cone-shaped bodies. 2004. Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.