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Investigation of AD-body interaction with microwave discharge region in supersonic flows. / Kolesnichenko, Yuri F.; Brovkin, Vadim G.; Leonov, Sergey B.; Krylov, Andrey A.; Lashkov, Valery A.; Mashek, Igor Ch; Gorynya, Anatoly A.; Ryvkin, Mark I.

2001. Работа представлена на 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, Соединенные Штаты Америки.

Результаты исследований: Материалы конференций › материалы › Рецензирование

Harvard

Kolesnichenko, YF, Brovkin, VG, Leonov, SB, Krylov, AA, Lashkov, VA, Mashek, IC, Gorynya, AA & Ryvkin, MI 2001, 'Investigation of AD-body interaction with microwave discharge region in supersonic flows', Работа представлена на 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, Соединенные Штаты Америки, 8/01/01 - 11/01/01.

APA

Kolesnichenko, Y. F., Brovkin, V. G., Leonov, S. B., Krylov, A. A., Lashkov, V. A., Mashek, I. C., Gorynya, A. A., & Ryvkin, M. I. (2001). Investigation of AD-body interaction with microwave discharge region in supersonic flows. Работа представлена на 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, Соединенные Штаты Америки.

Vancouver

Kolesnichenko YF, Brovkin VG, Leonov SB, Krylov AA, Lashkov VA, Mashek IC и пр.. Investigation of AD-body interaction with microwave discharge region in supersonic flows. 2001. Работа представлена на 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, Соединенные Штаты Америки.

Author

Kolesnichenko, Yuri F. ; Brovkin, Vadim G. ; Leonov, Sergey B. ; Krylov, Andrey A. ; Lashkov, Valery A. ; Mashek, Igor Ch ; Gorynya, Anatoly A. ; Ryvkin, Mark I. / Investigation of AD-body interaction with microwave discharge region in supersonic flows. Работа представлена на 39th Aerospace Sciences Meeting and Exhibit 2001, Reno, NV, Соединенные Штаты Америки.

BibTeX

@conference{db9c85d84dab4076abdba354cd966d85,
title = "Investigation of AD-body interaction with microwave discharge region in supersonic flows",
abstract = "The principle step in investigation of MW discharge in supersonic (SS) flows has been made. The detailed spatial-temporal data of discharge domains evolution and interaction with the BSW are obtained. They include synchronized information from optical emission diagnostics via using of hemiluminescence for discharge regions tracing, from the pressure sensors, which provide information about temporal evolution of the total pressure at stagnation point and Schlieren pictures available with time step of order of microsecond. Experiments were conducted under M-number 1.7-1.8 and peak MW power 210kW not only in airflow, but also in nitrogen, argon and carbon dioxide. All this, along with additional information about real discharge structure and gas temperatures in different plasmoids allowed to reconstruct the sequence of events in the process of discharge regions - AD model interaction, to formulate the regularities of such interaction and to eliminate those questions which are to be answered in further investigations.",
author = "Kolesnichenko, {Yuri F.} and Brovkin, {Vadim G.} and Leonov, {Sergey B.} and Krylov, {Andrey A.} and Lashkov, {Valery A.} and Mashek, {Igor Ch} and Gorynya, {Anatoly A.} and Ryvkin, {Mark I.}",
year = "2001",
month = dec,
day = "1",
language = "English",
note = "39th Aerospace Sciences Meeting and Exhibit 2001 ; Conference date: 08-01-2001 Through 11-01-2001",

}

RIS

TY - CONF

T1 - Investigation of AD-body interaction with microwave discharge region in supersonic flows

AU - Kolesnichenko, Yuri F.

AU - Brovkin, Vadim G.

AU - Leonov, Sergey B.

AU - Krylov, Andrey A.

AU - Lashkov, Valery A.

AU - Mashek, Igor Ch

AU - Gorynya, Anatoly A.

AU - Ryvkin, Mark I.

PY - 2001/12/1

Y1 - 2001/12/1

N2 - The principle step in investigation of MW discharge in supersonic (SS) flows has been made. The detailed spatial-temporal data of discharge domains evolution and interaction with the BSW are obtained. They include synchronized information from optical emission diagnostics via using of hemiluminescence for discharge regions tracing, from the pressure sensors, which provide information about temporal evolution of the total pressure at stagnation point and Schlieren pictures available with time step of order of microsecond. Experiments were conducted under M-number 1.7-1.8 and peak MW power 210kW not only in airflow, but also in nitrogen, argon and carbon dioxide. All this, along with additional information about real discharge structure and gas temperatures in different plasmoids allowed to reconstruct the sequence of events in the process of discharge regions - AD model interaction, to formulate the regularities of such interaction and to eliminate those questions which are to be answered in further investigations.

AB - The principle step in investigation of MW discharge in supersonic (SS) flows has been made. The detailed spatial-temporal data of discharge domains evolution and interaction with the BSW are obtained. They include synchronized information from optical emission diagnostics via using of hemiluminescence for discharge regions tracing, from the pressure sensors, which provide information about temporal evolution of the total pressure at stagnation point and Schlieren pictures available with time step of order of microsecond. Experiments were conducted under M-number 1.7-1.8 and peak MW power 210kW not only in airflow, but also in nitrogen, argon and carbon dioxide. All this, along with additional information about real discharge structure and gas temperatures in different plasmoids allowed to reconstruct the sequence of events in the process of discharge regions - AD model interaction, to formulate the regularities of such interaction and to eliminate those questions which are to be answered in further investigations.

UR - http://www.scopus.com/inward/record.url?scp=84897897707&partnerID=8YFLogxK

M3 - Paper

T2 - 39th Aerospace Sciences Meeting and Exhibit 2001

Y2 - 8 January 2001 through 11 January 2001

ER -

ID: 47782700