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Teplofizika vysokikh temperatur, 2022, Volume 60, Issue 1, Pages 153–155
DOI: https://doi.org/10.31857/S0040364422010239 (Mi tvt11269) 		 
This article is cited in 1 scientific paper (total in 1 paper)

Short Communications

The accuracy of hypersonic drag reduction test data: transient simulation and time constraints

A. M. Tahsinia, Anbuselvan K. K. N.b

a Iran University of Science & Technology
b Airbus India Private Limited, Bangalore, India
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DOI: https://doi.org/10.31857/S0040364422010239
Abstract: The method of using chromium coating for drag reduction of blunt bodies in hypersonic flow is numerically investigated using transient simulations. The focus is on the estimation of different time scales which are involved in the underlying physico-chemical processes. The results propose an appropriate timespan for the hypersonic test facilities to study such flow physics.
Received: 13.07.2019
Revised: 15.08.2020
Accepted: 02.02.2021
English version:
High Temperature, 2022, Volume 60, Issue 1, Pages 140–142
DOI: https://doi.org/10.1134/S0018151X22010175
Bibliographic databases:
Document Type: Article
UDC: 533.6.011.55, 6.013
Language: Russian
Citation: A. M. Tahsini, Anbuselvan K. K. N., “The accuracy of hypersonic drag reduction test data: transient simulation and time constraints”, TVT, 60:1 (2022), 153–155; High Temperature, 60:1 (2022), 140–142
Citation in format AMSBIB
\Bibitem{1}
\by A. M. Tahsini, Anbuselvan K. K. N.
\paper The accuracy of hypersonic drag reduction test data: transient simulation and time constraints
\jour TVT
\yr 2022
\vol 60
\issue 1
\pages 153--155
\mathnet{http://mi.mathnet.ru/tvt11269}
\crossref{https://doi.org/10.31857/S0040364422010239}
\elib{https://elibrary.ru/item.asp?id=48506044}
\transl
\jour High Temperature
\yr 2022
\vol 60
\issue 1
\pages 140--142
\crossref{https://doi.org/10.1134/S0018151X22010175}
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    • This publication is cited in the following 1 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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