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Investigation of heat flux on aerodynamic body in supersonic gas flow with local energy deposition. / Dobrov, Y. V.; Lashkov, V. A.; Mashek, I. Ch; Khoronzhuk, R. S.

In: AIP Conference Proceedings, Vol. 1959, 050009, 02.05.2018.

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@article{bae7f2b491f744378be4793a0e68e608,
title = "Investigation of heat flux on aerodynamic body in supersonic gas flow with local energy deposition",
abstract = "Existence and intensive growth of heat flux on a vehicle is one of the main problems in hypersonic flight. Experimental study of heat flux in the stagnation point of a blunt cylinder in supersonic flow was made using gradient heat flux sensor. It was found that a transfer function of the measuring system should be used for obtaining data at fast-changing heat flux measurements. It was established that it was possible to produce a short-term heat transfer from the surface of streamlined body with the help of microwave discharge. Numerical simulation showed that it is possible to change nature of the flow by means of local energy deposition in case of streamlined wedge.",
author = "Dobrov, {Y. V.} and Lashkov, {V. A.} and Mashek, {I. Ch} and Khoronzhuk, {R. S.}",
year = "2018",
month = may,
day = "2",
doi = "10.1063/1.5034637",
language = "English",
volume = "1959",
journal = "AIP Conference Proceedings",
issn = "0094-243X",
publisher = "American Institute of Physics",
note = "International Scientific Conference on Mechanics - Eighth Polyakhov's Reading : 8th Polyakhov's Reading ; Conference date: 29-01-2018 Through 02-02-2018",
url = "https://events.spbu.ru/events/polyakhov_readings, http://nanomat.spbu.ru/en/node/175, http://nanomat.spbu.ru/ru/node/192, http://spbu.ru/news-events/calendar/viii-polyahovskie-chteniya",

}

RIS

TY - JOUR

T1 - Investigation of heat flux on aerodynamic body in supersonic gas flow with local energy deposition

AU - Dobrov, Y. V.

AU - Lashkov, V. A.

AU - Mashek, I. Ch

AU - Khoronzhuk, R. S.

N1 - Conference code: 8

PY - 2018/5/2

Y1 - 2018/5/2

N2 - Existence and intensive growth of heat flux on a vehicle is one of the main problems in hypersonic flight. Experimental study of heat flux in the stagnation point of a blunt cylinder in supersonic flow was made using gradient heat flux sensor. It was found that a transfer function of the measuring system should be used for obtaining data at fast-changing heat flux measurements. It was established that it was possible to produce a short-term heat transfer from the surface of streamlined body with the help of microwave discharge. Numerical simulation showed that it is possible to change nature of the flow by means of local energy deposition in case of streamlined wedge.

AB - Existence and intensive growth of heat flux on a vehicle is one of the main problems in hypersonic flight. Experimental study of heat flux in the stagnation point of a blunt cylinder in supersonic flow was made using gradient heat flux sensor. It was found that a transfer function of the measuring system should be used for obtaining data at fast-changing heat flux measurements. It was established that it was possible to produce a short-term heat transfer from the surface of streamlined body with the help of microwave discharge. Numerical simulation showed that it is possible to change nature of the flow by means of local energy deposition in case of streamlined wedge.

UR - http://www.scopus.com/inward/record.url?scp=85047178767&partnerID=8YFLogxK

U2 - 10.1063/1.5034637

DO - 10.1063/1.5034637

M3 - Conference article

AN - SCOPUS:85047178767

VL - 1959

JO - AIP Conference Proceedings

JF - AIP Conference Proceedings

SN - 0094-243X

M1 - 050009

T2 - International Scientific Conference on Mechanics - Eighth Polyakhov's Reading

Y2 - 29 January 2018 through 2 February 2018

ER -

ID: 36759798