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Teplofizika vysokikh temperatur, 2020, Volume 58, Issue 2, Pages 175–178
DOI: https://doi.org/10.31857/S0040364420020118 (Mi tvt11221) 		 
This article is cited in 2 scientific papers (total in 2 papers)

Plasma Investigations

Probe measurements on board a hypersonic aircraft

V. A. Kotel'nikovab, M. V. Kotelnikovab, D. V. Kassinab

a Moscow Aviation Institute, USSR
b A. A. Blagonravov Mechanical Engineering Institute RAS, Moscow
Full-text PDF (592 kB) Citations (2)
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DOI: https://doi.org/10.31857/S0040364420020118
Abstract: The features of probe measurements on a hypersonic aircraft, the design of the probe block and its location on a hypersonic aircraft, and the processing technique of the obtained current-voltage characteristics are discussed. Original processing techniques are proposed, and some results of probe measurements, covering both the plasma parameters in the combustion products of a liquid propellant rocket engine and the parameters of the plasma arising at supersonic speeds near the hypersonic aircraft wall, are presented.
Received: 17.04.2019
Revised: 05.10.2019
Accepted: 22.10.2019
English version:
High Temperature, 2020, Volume 58, Issue 2, Pages 162–165
DOI: https://doi.org/10.1134/S0018151X2002011X
Bibliographic databases:
Document Type: Article
UDC: 533
Language: Russian
Citation: V. A. Kotel'nikov, M. V. Kotelnikov, D. V. Kassin, “Probe measurements on board a hypersonic aircraft”, TVT, 58:2 (2020), 175–178; High Temperature, 58:2 (2020), 162–165
Citation in format AMSBIB
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\paper Probe measurements on board a~hypersonic aircraft
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    • This publication is cited in the following 2 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Teplofizika vysokikh temperatur Teplofizika vysokikh temperatur
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