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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 Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.

Research output: Contribution to conferencePaperpeer-review

Harvard

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', Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, 5/01/04 - 8/01/04 pp. 1536-1550.

APA

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. Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.

Vancouver

Kolesnichcnko YF, Azarova OA, Brovkin VG, Khmara DV, Lashkov VA, Mashek IC et al. Basics in beamed MW energy deposition for flow/flight control. 2004. Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.

Author

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. Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.15 p.

BibTeX

@conference{53e69caa48724ef197d755347cf089e8,
title = "Basics in beamed MW energy deposition for flow/flight control",
abstract = "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.",
author = "Kolesnichcnko, {Yuri F.} and Azarova, {Olga A.} and Brovkin, {Vadim G.} and Khmara, {Dmitry V.} and Lashkov, {Valery A.} and Mashek, {Igor Ch} and Ryvkin, {Mark I.}",
year = "2004",
month = jul,
day = "1",
language = "English",
pages = "1536--1550",
note = "42nd AIAA Aerospace Sciences Meeting and Exhibit ; Conference date: 05-01-2004 Through 08-01-2004",

}

RIS

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.

UR - http://www.scopus.com/inward/record.url?scp=2942735174&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:2942735174

SP - 1536

EP - 1550

T2 - 42nd AIAA Aerospace Sciences Meeting and Exhibit

Y2 - 5 January 2004 through 8 January 2004

ER -

ID: 47781415