Basics in beamed MW energy deposition for flow/flight control

Yuri F. Kolesnichcnko, Olga A. Azarova, Vadim G. Brovkin, Dmitry V. Khmara, Valery A. Lashkov, Igor Ch Mashek, Mark I. Ryvkin

Результат исследований: Материалы конференцийматериалы

14 Цитирования (Scopus)

Выдержка

Present investigation is focused on formulation of valid and realistic physical basis in exploration of the challenging phenomenon in plasma aerodynamics - interference of MW discharge with gas dynamic structures in supersonic flow. We now distinguish three basic phenomena, reflecting the main features of such interference. These phenomena - drag reduction via discharge-induced vortex creation in a shock layer, regular-Mach discharge-induced transition in intersecting shocks and radical change in flow separation in streamlining of spike-tipped bodies through discharge-affecting of viscous interaction - cover the most impressive areas of plasma aerodynamics and at the same time form its basis. Each of these examples demonstrates wide abilities of MW energy deposition method and presents the complicated physics, which is not fully understood yet. Also discharge structure plays a key role in effective interaction with gas dynamic discontinuities. The parameters of MW plasmoid internal structure are quantified, the principle of information extraction from spectra of strongly inhomogeneous plasma objects is proposed. Discharge performance requirements are formulated Beamed energy deposition as a principle tool for plasma aerodynamic phenomena realization seems both claimed and inherent and in general demands application combined MW and laser techniques.

Язык оригиналаанглийский
Страницы1536-1550
Число страниц15
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

Plasmas
Aerodynamics
Gas dynamics
Discharge (fluid mechanics)
Drag reduction
Supersonic flow
Flow separation
Beam plasma interactions
Mach number
Vortex flow
Physics
Lasers

Предметные области Scopus

  • Технология (все)

Цитировать

Kolesnichcnko, Y. F., Azarova, O. A., Brovkin, V. G., Khmara, D. V., Lashkov, V. A., Mashek, I. C., & Ryvkin, M. I. (2004). Basics in beamed MW energy deposition for flow/flight control. 1536-1550. Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.
Kolesnichcnko, Yuri F. ; Azarova, Olga A. ; Brovkin, Vadim G. ; Khmara, Dmitry V. ; Lashkov, Valery A. ; Mashek, Igor Ch ; Ryvkin, Mark I. / Basics in beamed MW energy deposition for flow/flight control. Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.15 стр.
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Kolesnichcnko, YF, Azarova, OA, Brovkin, VG, Khmara, DV, Lashkov, VA, Mashek, IC & Ryvkin, MI 2004, 'Basics in beamed MW energy deposition for flow/flight control' Документ представлен на, Reno, NV, Соединенные Штаты Америки, 5/01/04 - 8/01/04, стр. 1536-1550.

Basics in beamed MW energy deposition for flow/flight control. / Kolesnichcnko, Yuri F.; Azarova, Olga A.; Brovkin, Vadim G.; Khmara, Dmitry V.; Lashkov, Valery A.; Mashek, Igor Ch; Ryvkin, Mark I.

2004. 1536-1550 Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.

Результат исследований: Материалы конференцийматериалы

TY - CONF

T1 - Basics in beamed MW energy deposition for flow/flight control

AU - Kolesnichcnko, Yuri F.

AU - Azarova, Olga A.

AU - Brovkin, Vadim G.

AU - Khmara, Dmitry V.

AU - Lashkov, Valery A.

AU - Mashek, Igor Ch

AU - Ryvkin, Mark I.

PY - 2004/7/1

Y1 - 2004/7/1

N2 - Present investigation is focused on formulation of valid and realistic physical basis in exploration of the challenging phenomenon in plasma aerodynamics - interference of MW discharge with gas dynamic structures in supersonic flow. We now distinguish three basic phenomena, reflecting the main features of such interference. These phenomena - drag reduction via discharge-induced vortex creation in a shock layer, regular-Mach discharge-induced transition in intersecting shocks and radical change in flow separation in streamlining of spike-tipped bodies through discharge-affecting of viscous interaction - cover the most impressive areas of plasma aerodynamics and at the same time form its basis. Each of these examples demonstrates wide abilities of MW energy deposition method and presents the complicated physics, which is not fully understood yet. Also discharge structure plays a key role in effective interaction with gas dynamic discontinuities. The parameters of MW plasmoid internal structure are quantified, the principle of information extraction from spectra of strongly inhomogeneous plasma objects is proposed. Discharge performance requirements are formulated Beamed energy deposition as a principle tool for plasma aerodynamic phenomena realization seems both claimed and inherent and in general demands application combined MW and laser techniques.

AB - Present investigation is focused on formulation of valid and realistic physical basis in exploration of the challenging phenomenon in plasma aerodynamics - interference of MW discharge with gas dynamic structures in supersonic flow. We now distinguish three basic phenomena, reflecting the main features of such interference. These phenomena - drag reduction via discharge-induced vortex creation in a shock layer, regular-Mach discharge-induced transition in intersecting shocks and radical change in flow separation in streamlining of spike-tipped bodies through discharge-affecting of viscous interaction - cover the most impressive areas of plasma aerodynamics and at the same time form its basis. Each of these examples demonstrates wide abilities of MW energy deposition method and presents the complicated physics, which is not fully understood yet. Also discharge structure plays a key role in effective interaction with gas dynamic discontinuities. The parameters of MW plasmoid internal structure are quantified, the principle of information extraction from spectra of strongly inhomogeneous plasma objects is proposed. Discharge performance requirements are formulated Beamed energy deposition as a principle tool for plasma aerodynamic phenomena realization seems both claimed and inherent and in general demands application combined MW and laser techniques.

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Kolesnichcnko YF, Azarova OA, Brovkin VG, Khmara DV, Lashkov VA, Mashek IC и соавт.. Basics in beamed MW energy deposition for flow/flight control. 2004. Документ представлен на 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки.