Plasma actuator for supersonic flows based on miniature magneto-plasma compressor

Результат исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийстатья в сборнике материалов конференциинаучнаярецензирование

2 Цитирования (Scopus)

Выдержка

Investigations of Large-Scale Magneto-Plasma Compressor (L-S MPC), performed in our previous works show, that L-S MPC (outlet diameter 40 mm), operated in High-Pressure Residual Gas Regime (HPRGR) could generate comparatively long-lived (jet lifetime 50-70 μs) hypersonic plasma jets (Mach number 4,5-5) with high density (up to 1017 cm-3), temperature (up to 3 eV) and penetration ability (stagnation pressure more than 150 bar). These jets could be useful in applied plasmadynamics for development of a new type of plasma actuator for injection of high-enthalpy plasma jets both into quiescent gas and in supersonic flows with static pressure up to 100 Torr. Unfortunately, the energy characteristics of L-S-MPC are not suitable for real practical applications. It was the reason why the creation of miniature MPC with comparatively low input energy becomes very important. In the presented work the simplest model of Miniature MPC (MMPC) with effective outlet diameter 14 mm was constructed and examined. The results of these investigations demonstrate that MPC in mini-size variant operated in HPRGR has the similar mechanisms of jet arising as it large-scale analog, but with dramatically decreased input energetic characteristics (15-20 J/pulse for MMPC versus 0,6-1,5 kJ/pulse for L-S MPC). The last fact gives the opportunity for MMPC using as base element in possible constructions of array plasma injectors.

Язык оригиналаанглийский
Название основной публикации46th AIAA Aerospace Sciences Meeting and Exhibit
СостояниеОпубликовано - 1 дек 2008
Событие46th AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, Соединенные Штаты Америки
Продолжительность: 7 янв 200810 янв 2008

Серия публикаций

Название46th AIAA Aerospace Sciences Meeting and Exhibit

Конференция

Конференция46th AIAA Aerospace Sciences Meeting and Exhibit
СтранаСоединенные Штаты Америки
ГородReno, NV
Период7/01/0810/01/08

Отпечаток

Supersonic flow
Compressors
Actuators
Plasmas
Plasma jets
Gases
Hypersonic aerodynamics
Mach number
Enthalpy
Temperature

Предметные области Scopus

  • Авиакосмическая техника

Цитировать

Mashek, I. C., Anisimov, Y. I., Lashkov, V. A., & Kolesnichenko, Y. F. (2008). Plasma actuator for supersonic flows based on miniature magneto-plasma compressor. В 46th AIAA Aerospace Sciences Meeting and Exhibit [2008-1408] (46th AIAA Aerospace Sciences Meeting and Exhibit).
Mashek, I. Ch ; Anisimov, Yu I. ; Lashkov, V. A. ; Kolesnichenko, Yu F. / Plasma actuator for supersonic flows based on miniature magneto-plasma compressor. 46th AIAA Aerospace Sciences Meeting and Exhibit. 2008. (46th AIAA Aerospace Sciences Meeting and Exhibit).
@inproceedings{02fbfbf448284247ad4e7230bcf03c4b,
title = "Plasma actuator for supersonic flows based on miniature magneto-plasma compressor",
abstract = "Investigations of Large-Scale Magneto-Plasma Compressor (L-S MPC), performed in our previous works show, that L-S MPC (outlet diameter 40 mm), operated in High-Pressure Residual Gas Regime (HPRGR) could generate comparatively long-lived (jet lifetime 50-70 μs) hypersonic plasma jets (Mach number 4,5-5) with high density (up to 1017 cm-3), temperature (up to 3 eV) and penetration ability (stagnation pressure more than 150 bar). These jets could be useful in applied plasmadynamics for development of a new type of plasma actuator for injection of high-enthalpy plasma jets both into quiescent gas and in supersonic flows with static pressure up to 100 Torr. Unfortunately, the energy characteristics of L-S-MPC are not suitable for real practical applications. It was the reason why the creation of miniature MPC with comparatively low input energy becomes very important. In the presented work the simplest model of Miniature MPC (MMPC) with effective outlet diameter 14 mm was constructed and examined. The results of these investigations demonstrate that MPC in mini-size variant operated in HPRGR has the similar mechanisms of jet arising as it large-scale analog, but with dramatically decreased input energetic characteristics (15-20 J/pulse for MMPC versus 0,6-1,5 kJ/pulse for L-S MPC). The last fact gives the opportunity for MMPC using as base element in possible constructions of array plasma injectors.",
author = "Mashek, {I. Ch} and Anisimov, {Yu I.} and Lashkov, {V. A.} and Kolesnichenko, {Yu F.}",
year = "2008",
month = "12",
day = "1",
language = "English",
isbn = "9781563479373",
series = "46th AIAA Aerospace Sciences Meeting and Exhibit",
booktitle = "46th AIAA Aerospace Sciences Meeting and Exhibit",

}

Mashek, IC, Anisimov, YI, Lashkov, VA & Kolesnichenko, YF 2008, Plasma actuator for supersonic flows based on miniature magneto-plasma compressor. в 46th AIAA Aerospace Sciences Meeting and Exhibit., 2008-1408, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Соединенные Штаты Америки, 7/01/08.

Plasma actuator for supersonic flows based on miniature magneto-plasma compressor. / Mashek, I. Ch; Anisimov, Yu I.; Lashkov, V. A.; Kolesnichenko, Yu F.

46th AIAA Aerospace Sciences Meeting and Exhibit. 2008. 2008-1408 (46th AIAA Aerospace Sciences Meeting and Exhibit).

Результат исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийстатья в сборнике материалов конференциинаучнаярецензирование

TY - GEN

T1 - Plasma actuator for supersonic flows based on miniature magneto-plasma compressor

AU - Mashek, I. Ch

AU - Anisimov, Yu I.

AU - Lashkov, V. A.

AU - Kolesnichenko, Yu F.

PY - 2008/12/1

Y1 - 2008/12/1

N2 - Investigations of Large-Scale Magneto-Plasma Compressor (L-S MPC), performed in our previous works show, that L-S MPC (outlet diameter 40 mm), operated in High-Pressure Residual Gas Regime (HPRGR) could generate comparatively long-lived (jet lifetime 50-70 μs) hypersonic plasma jets (Mach number 4,5-5) with high density (up to 1017 cm-3), temperature (up to 3 eV) and penetration ability (stagnation pressure more than 150 bar). These jets could be useful in applied plasmadynamics for development of a new type of plasma actuator for injection of high-enthalpy plasma jets both into quiescent gas and in supersonic flows with static pressure up to 100 Torr. Unfortunately, the energy characteristics of L-S-MPC are not suitable for real practical applications. It was the reason why the creation of miniature MPC with comparatively low input energy becomes very important. In the presented work the simplest model of Miniature MPC (MMPC) with effective outlet diameter 14 mm was constructed and examined. The results of these investigations demonstrate that MPC in mini-size variant operated in HPRGR has the similar mechanisms of jet arising as it large-scale analog, but with dramatically decreased input energetic characteristics (15-20 J/pulse for MMPC versus 0,6-1,5 kJ/pulse for L-S MPC). The last fact gives the opportunity for MMPC using as base element in possible constructions of array plasma injectors.

AB - Investigations of Large-Scale Magneto-Plasma Compressor (L-S MPC), performed in our previous works show, that L-S MPC (outlet diameter 40 mm), operated in High-Pressure Residual Gas Regime (HPRGR) could generate comparatively long-lived (jet lifetime 50-70 μs) hypersonic plasma jets (Mach number 4,5-5) with high density (up to 1017 cm-3), temperature (up to 3 eV) and penetration ability (stagnation pressure more than 150 bar). These jets could be useful in applied plasmadynamics for development of a new type of plasma actuator for injection of high-enthalpy plasma jets both into quiescent gas and in supersonic flows with static pressure up to 100 Torr. Unfortunately, the energy characteristics of L-S-MPC are not suitable for real practical applications. It was the reason why the creation of miniature MPC with comparatively low input energy becomes very important. In the presented work the simplest model of Miniature MPC (MMPC) with effective outlet diameter 14 mm was constructed and examined. The results of these investigations demonstrate that MPC in mini-size variant operated in HPRGR has the similar mechanisms of jet arising as it large-scale analog, but with dramatically decreased input energetic characteristics (15-20 J/pulse for MMPC versus 0,6-1,5 kJ/pulse for L-S MPC). The last fact gives the opportunity for MMPC using as base element in possible constructions of array plasma injectors.

UR - http://www.scopus.com/inward/record.url?scp=78149463546&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:78149463546

SN - 9781563479373

T3 - 46th AIAA Aerospace Sciences Meeting and Exhibit

BT - 46th AIAA Aerospace Sciences Meeting and Exhibit

ER -

Mashek IC, Anisimov YI, Lashkov VA, Kolesnichenko YF. Plasma actuator for supersonic flows based on miniature magneto-plasma compressor. В 46th AIAA Aerospace Sciences Meeting and Exhibit. 2008. 2008-1408. (46th AIAA Aerospace Sciences Meeting and Exhibit).