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Thermal modeling for the sustained hypersonic flight experiment

Abstract:

This paper details the development, validation, and use of a thermal model created to predict the surface temperatures through the U.K. Ministry of Defence funded sustained hypersonic flight experiment ramjet vehicle. The sustained hypersonic flight experiment ramjet will operate at Mach 4 to 6 leading to very high airflow stagnation temperatures. It was therefore important to predict the temperatures during the flight experiment at an early design stage, before the vehicle geometry was final...

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Publication status:
Published

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Publisher copy:
10.2514/1.29317

Authors


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Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
Journal:
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
Volume:
21
Issue:
4
Pages:
780-789
Publication date:
2007-01-01
DOI:
EISSN:
1533-6808
ISSN:
0887-8722
Source identifiers:
288953
Language:
English
Pubs id:
pubs:288953
UUID:
uuid:c32bb772-e81f-4fcb-833d-e48c50bd1a76
Local pid:
pubs:288953
Deposit date:
2012-12-19

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