Calculation of heat transfer on the catalytically active surface of high-speed aircraft
The scientific paper analyzes the influence of the catalytically active surface on the intensity of heat and mass transfer in a chemically active boundary layer. Some features of the mechanism of heat and mass transfer under conditions of heterogeneous catalysis are indicated. Heat transfer analysis...
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2019-08-01
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doaj-75f94d5af0a347259706c36592365e202020-11-25T01:43:07ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282019-08-0111S19120110.13111/2066-8201.2019.11.S.19Calculation of heat transfer on the catalytically active surface of high-speed aircraftPetr V. NIKITIN0Olga V. TUSHAVINA1Anna A. SHKURATENKO2Institute of Aerospace, Moscow Aviation Institute (National Research University), 4 Volokolamskoe Highway, 125993, Moscow, Russian Federation, petrunecha@gmail.comInstitute of Aerospace, Moscow Aviation Institute (National Research University), 4 Volokolamskoe Highway, 125993, Moscow, Russian Federation, solgtu@gmail.comInstitute of Aerospace, Moscow Aviation Institute (National Research University), 4 Volokolamskoe Highway, 125993, Moscow, Russian Federation, shkuratenko.anna@mail.ruThe scientific paper analyzes the influence of the catalytically active surface on the intensity of heat and mass transfer in a chemically active boundary layer. Some features of the mechanism of heat and mass transfer under conditions of heterogeneous catalysis are indicated. Heat transfer analysis is performed in the laminar “frozen” boundary layer with zero and absolute catalytic surface activity. In order to improve the accuracy of the calculation of heat fluxes on the catalytically active surface, a modification of the Gullard ratio is carried out. Using the modified Gullard ratio obtained in this work, calculations of heat transfer on a catalytically active surface are carried out. It is shown that the levels of heat fluxes calculated using a modified ratio of up to 30% below the levels of heat fluxes obtained from the Gullard ratio under otherwise equal conditions.high-temperature flowspacecraftchemically active boundary layerdissociation reactions |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Petr V. NIKITIN Olga V. TUSHAVINA Anna A. SHKURATENKO |
spellingShingle |
Petr V. NIKITIN Olga V. TUSHAVINA Anna A. SHKURATENKO Calculation of heat transfer on the catalytically active surface of high-speed aircraft INCAS Bulletin high-temperature flow spacecraft chemically active boundary layer dissociation reactions |
author_facet |
Petr V. NIKITIN Olga V. TUSHAVINA Anna A. SHKURATENKO |
author_sort |
Petr V. NIKITIN |
title |
Calculation of heat transfer on the catalytically active surface of high-speed aircraft |
title_short |
Calculation of heat transfer on the catalytically active surface of high-speed aircraft |
title_full |
Calculation of heat transfer on the catalytically active surface of high-speed aircraft |
title_fullStr |
Calculation of heat transfer on the catalytically active surface of high-speed aircraft |
title_full_unstemmed |
Calculation of heat transfer on the catalytically active surface of high-speed aircraft |
title_sort |
calculation of heat transfer on the catalytically active surface of high-speed aircraft |
publisher |
National Institute for Aerospace Research “Elie Carafoli” - INCAS |
series |
INCAS Bulletin |
issn |
2066-8201 2247-4528 |
publishDate |
2019-08-01 |
description |
The scientific paper analyzes the influence of the catalytically active surface on the intensity of heat and mass transfer in a chemically active boundary layer. Some features of the mechanism of heat and mass transfer under conditions of heterogeneous catalysis are indicated. Heat transfer analysis is performed in the laminar “frozen” boundary layer with zero and absolute catalytic surface activity. In order to improve the accuracy of the calculation of heat fluxes on the catalytically active surface, a modification of the Gullard ratio is carried out. Using the modified Gullard ratio obtained in this work, calculations of heat transfer on a catalytically active surface are carried out. It is shown that the levels of heat fluxes calculated using a modified ratio of up to 30% below the levels of heat fluxes obtained from the Gullard ratio under otherwise equal conditions. |
topic |
high-temperature flow spacecraft chemically active boundary layer dissociation reactions |
work_keys_str_mv |
AT petrvnikitin calculationofheattransferonthecatalyticallyactivesurfaceofhighspeedaircraft AT olgavtushavina calculationofheattransferonthecatalyticallyactivesurfaceofhighspeedaircraft AT annaashkuratenko calculationofheattransferonthecatalyticallyactivesurfaceofhighspeedaircraft |
_version_ |
1725033203682508800 |