Standard

Improvement of aircraft aerodynamic properties by energy supply into airflow when using highly efficient plasma generators. / Ivanov, V. A.; Kuchinskiy, V. V.; Kuranov, A. L.; Sukhomlinov, V. S.

42nd AIAA Aerospace Sciences Meeting and Exhibit. 2004. p. 1173-1181.

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Harvard

Ivanov, VA, Kuchinskiy, VV, Kuranov, AL & Sukhomlinov, VS 2004, Improvement of aircraft aerodynamic properties by energy supply into airflow when using highly efficient plasma generators. in 42nd AIAA Aerospace Sciences Meeting and Exhibit. pp. 1173-1181, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, 5/01/04.

APA

Ivanov, V. A., Kuchinskiy, V. V., Kuranov, A. L., & Sukhomlinov, V. S. (2004). Improvement of aircraft aerodynamic properties by energy supply into airflow when using highly efficient plasma generators. In 42nd AIAA Aerospace Sciences Meeting and Exhibit (pp. 1173-1181)

Vancouver

Ivanov VA, Kuchinskiy VV, Kuranov AL, Sukhomlinov VS. Improvement of aircraft aerodynamic properties by energy supply into airflow when using highly efficient plasma generators. In 42nd AIAA Aerospace Sciences Meeting and Exhibit. 2004. p. 1173-1181

Author

Ivanov, V. A. ; Kuchinskiy, V. V. ; Kuranov, A. L. ; Sukhomlinov, V. S. / Improvement of aircraft aerodynamic properties by energy supply into airflow when using highly efficient plasma generators. 42nd AIAA Aerospace Sciences Meeting and Exhibit. 2004. pp. 1173-1181

BibTeX

@inproceedings{28a9cce16d7a46a2aae07a822fe9fc0a,
title = "Improvement of aircraft aerodynamic properties by energy supply into airflow when using highly efficient plasma generators",
abstract = "The development of physical foundations and approptiate gear, as well as experimental testing of the concept of local energy forcing on high-speed gas streams aimed to improve aerodynamic properties of streamlined bodies is described. According to thermodynamics of gas flows, supply of energy to the subsonic stream increases Mach number, while energy supply to the supersonic flow decreases it. The development of a principally new generator of independent plasma discharge with high frequency of consumed energy transformation and high stability of plasma parameters is also discussed.",
author = "Ivanov, {V. A.} and Kuchinskiy, {V. V.} and Kuranov, {A. L.} and Sukhomlinov, {V. S.}",
year = "2004",
language = "English",
pages = "1173--1181",
booktitle = "42nd AIAA Aerospace Sciences Meeting and Exhibit",
note = "42nd AIAA Aerospace Sciences Meeting and Exhibit ; Conference date: 05-01-2004 Through 08-01-2004",

}

RIS

TY - GEN

T1 - Improvement of aircraft aerodynamic properties by energy supply into airflow when using highly efficient plasma generators

AU - Ivanov, V. A.

AU - Kuchinskiy, V. V.

AU - Kuranov, A. L.

AU - Sukhomlinov, V. S.

PY - 2004

Y1 - 2004

N2 - The development of physical foundations and approptiate gear, as well as experimental testing of the concept of local energy forcing on high-speed gas streams aimed to improve aerodynamic properties of streamlined bodies is described. According to thermodynamics of gas flows, supply of energy to the subsonic stream increases Mach number, while energy supply to the supersonic flow decreases it. The development of a principally new generator of independent plasma discharge with high frequency of consumed energy transformation and high stability of plasma parameters is also discussed.

AB - The development of physical foundations and approptiate gear, as well as experimental testing of the concept of local energy forcing on high-speed gas streams aimed to improve aerodynamic properties of streamlined bodies is described. According to thermodynamics of gas flows, supply of energy to the subsonic stream increases Mach number, while energy supply to the supersonic flow decreases it. The development of a principally new generator of independent plasma discharge with high frequency of consumed energy transformation and high stability of plasma parameters is also discussed.

UR - http://www.scopus.com/inward/record.url?scp=2942720632&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:2942720632

SP - 1173

EP - 1181

BT - 42nd AIAA Aerospace Sciences Meeting and Exhibit

T2 - 42nd AIAA Aerospace Sciences Meeting and Exhibit

Y2 - 5 January 2004 through 8 January 2004

ER -

ID: 9653292