Journal article
Flow characterization of porous ultra-high-temperature ceramics for transpiration cooling
- Abstract:
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Porous ultra-high-temperature ceramics (UHTCs) are a candidate group of materials for transpiration cooling of hypersonic vehicles due to their exceptionally high melting point, typically above 3000 K. Their high operating temperature permits a higher amount of radiative cooling than that achievable with conventional materials, which reduces the required coolant mass flow rate to cool the surface. This work experimentally examines the internal and external flow behavior of porous UHTC made of...
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- Publication status:
- Published
- Peer review status:
- Peer reviewed
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- Files:
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(Accepted manuscript, 9.7MB)
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- Publisher copy:
- 10.2514/1.J061009
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Authors
Funding
Bibliographic Details
- Publisher:
- American Institute of Aeronautics and Astronautics Publisher's website
- Journal:
- AIAA JOURNAL
- Volume:
- 60
- Issue:
- 5
- Pages:
- 3286-3297
- Publication date:
- 2022-02-28
- DOI:
- EISSN:
-
1533-385X
- ISSN:
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0001-1452
Item Description
- Language:
- English
- Keywords:
- Pubs id:
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1249387
- Local pid:
- pubs:1249387
- Deposit date:
- 2022-06-26
Terms of use
- Copyright holder:
- Ifti et al.
- Copyright date:
- 2022
- Rights statement:
- ©2022 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
- Notes:
- This is the accepted manuscript version of the article. The final version is available from the American Institute of Aeronautics and Astronautics at: 10.2514/1.J061009
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