Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer

A. D. Kosinov; G. L. Kolosov; A. A. Yatskikh; N. V. Semionov; Yu G. Yermolaev; A. V. Panina

doi:10.1063/1.5065094

Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer

A. D. Kosinov, G. L. Kolosov, A. A. Yatskikh, N. V. Semionov, Yu G. Yermolaev, A. V. Panina

Результат исследования: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › рецензирование

3 Цитирования (Scopus)

Аннотация

The paper is devoted to the experimental study of the growth of mass flux pulsations and disturbances of total temperature at the laminar-turbulent transition process in a modulated swept-wing boundary layer at Mach number of the oncoming flow M = 2 and 2.5. Total temperature and mass flow pulsations were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. It was found that at laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.

Язык оригинала	английский
Название основной публикации	19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
Редакторы	Fomin
Издатель	American Institute of Physics Inc.
Число страниц	4
Том	2027
ISBN (электронное издание)	9780735417472
DOI	https://doi.org/10.1063/1.5065094
Состояние	Опубликовано - 2 ноя 2018
Событие	19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 - Akademgorodok, Novosibirsk, Российская Федерация Продолжительность: 13 авг 2018 → 19 авг 2018

Серия публикаций

Название	AIP Conference Proceedings
Издатель	AMER INST PHYSICS
Том	2027
ISSN (печатное издание)	0094-243X

Конференция

Конференция	19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
Страна	Российская Федерация
Город	Akademgorodok, Novosibirsk
Период	13.08.2018 → 19.08.2018

Доступ к документу

10.1063/1.5065094

Link to publication in Scopus

Fingerprint Подробные сведения о темах исследования «Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer». Вместе они формируют уникальный семантический отпечаток (fingerprint).

Цитировать

Kosinov, A. D., Kolosov, G. L., Yatskikh, A. A., Semionov, N. V., Yermolaev, Y. G., & Panina, A. V. (2018). Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. В Fomin (Ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Том 2027). [020016] (AIP Conference Proceedings; Том 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065094

Kosinov, A. D. ; Kolosov, G. L. ; Yatskikh, A. A. ; Semionov, N. V. ; Yermolaev, Yu G. ; Panina, A. V. / Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. редактор / Fomin. Том 2027 American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

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title = "Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer",

abstract = "The paper is devoted to the experimental study of the growth of mass flux pulsations and disturbances of total temperature at the laminar-turbulent transition process in a modulated swept-wing boundary layer at Mach number of the oncoming flow M = 2 and 2.5. Total temperature and mass flow pulsations were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. It was found that at laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.",

author = "Kosinov, {A. D.} and Kolosov, {G. L.} and Yatskikh, {A. A.} and Semionov, {N. V.} and Yermolaev, {Yu G.} and Panina, {A. V.}",

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publisher = "American Institute of Physics Inc.",

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note = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 ; Conference date: 13-08-2018 Through 19-08-2018",

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Kosinov, AD, Kolosov, GL, Yatskikh, AA, Semionov, NV, Yermolaev, YG & Panina, AV 2018, Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. в Fomin (ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. том. 2027, 020016, AIP Conference Proceedings, том. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Российская Федерация, 13.08.2018. https://doi.org/10.1063/1.5065094

Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. / Kosinov, A. D.; Kolosov, G. L.; Yatskikh, A. A.; Semionov, N. V.; Yermolaev, Yu G.; Panina, A. V.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Fomin. Том 2027 American Institute of Physics Inc., 2018. 020016 (AIP Conference Proceedings; Том 2027).

Результат исследования: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › рецензирование

TY - GEN

T1 - Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer

AU - Kosinov, A. D.

AU - Kolosov, G. L.

AU - Yatskikh, A. A.

AU - Semionov, N. V.

AU - Yermolaev, Yu G.

AU - Panina, A. V.

PY - 2018/11/2

Y1 - 2018/11/2

N2 - The paper is devoted to the experimental study of the growth of mass flux pulsations and disturbances of total temperature at the laminar-turbulent transition process in a modulated swept-wing boundary layer at Mach number of the oncoming flow M = 2 and 2.5. Total temperature and mass flow pulsations were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. It was found that at laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.

AB - The paper is devoted to the experimental study of the growth of mass flux pulsations and disturbances of total temperature at the laminar-turbulent transition process in a modulated swept-wing boundary layer at Mach number of the oncoming flow M = 2 and 2.5. Total temperature and mass flow pulsations were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. It was found that at laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.

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PB - American Institute of Physics Inc.

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Kosinov AD, Kolosov GL, Yatskikh AA, Semionov NV, Yermolaev YG, Panina AV. Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. В Fomin, редактор, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том 2027. American Institute of Physics Inc. 2018. 020016. (AIP Conference Proceedings). https://doi.org/10.1063/1.5065094