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Influences of accelerating states on supercritical n-decane heat transfer in a horizontal tube applied for scramjet engine cooling

Chen, Youqian ; Li, Yong LU orcid ; Liu, Dechao ; Sunden, Bengt LU and Xie, Gongnan LU (2021) In Aerospace Science and Technology 109.
Abstract

Supercritical n-decane is applied in the regenerative cooling system of scramjet engines while scramjets are always in various irregular movements. With the desire to explore heat transfer performance of supercritical n-decane under actual flight conditions, numerical simulations and analysis of different states during the accelerated flight process are carried out under three different heat fluxes and eight varying acceleration states. Specific flow and heat transfer mechanisms are explored by analyzing the temperature and flow fields affected by acceleration. Results show that acceleration weakens the intensity of the first abnormal heat transfer state but does not affect its appearance location, and there are almost no effects on the... (More)

Supercritical n-decane is applied in the regenerative cooling system of scramjet engines while scramjets are always in various irregular movements. With the desire to explore heat transfer performance of supercritical n-decane under actual flight conditions, numerical simulations and analysis of different states during the accelerated flight process are carried out under three different heat fluxes and eight varying acceleration states. Specific flow and heat transfer mechanisms are explored by analyzing the temperature and flow fields affected by acceleration. Results show that acceleration weakens the intensity of the first abnormal heat transfer state but does not affect its appearance location, and there are almost no effects on the second heat transfer state. Another important conclusion is that the external factors have a great influence on supercritical n-decane heat transfer. The overall average surface heat transfer coefficient could be even up to 27.5% higher than for an ordinary horizontal tube. It is indicated that more attention should be paid to the external factors when investigating supercritical flow and heat transfer in the research and development of scramjet engine cooling.

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author
; ; ; and
organization
publishing date
type
Contribution to journal
publication status
published
subject
keywords
Acceleration, Buoyancy, External factors, Heat transfer coefficient, Supercritical n-decane
in
Aerospace Science and Technology
volume
109
article number
106424
publisher
Elsevier Masson SAS
external identifiers
  • scopus:85098456194
ISSN
1270-9638
DOI
10.1016/j.ast.2020.106424
language
English
LU publication?
yes
id
c6189e71-f29e-4899-905d-bb6eff5714c8
date added to LUP
2021-12-22 11:21:43
date last changed
2023-11-09 02:14:58
@article{c6189e71-f29e-4899-905d-bb6eff5714c8,
  abstract     = {{<p>Supercritical n-decane is applied in the regenerative cooling system of scramjet engines while scramjets are always in various irregular movements. With the desire to explore heat transfer performance of supercritical n-decane under actual flight conditions, numerical simulations and analysis of different states during the accelerated flight process are carried out under three different heat fluxes and eight varying acceleration states. Specific flow and heat transfer mechanisms are explored by analyzing the temperature and flow fields affected by acceleration. Results show that acceleration weakens the intensity of the first abnormal heat transfer state but does not affect its appearance location, and there are almost no effects on the second heat transfer state. Another important conclusion is that the external factors have a great influence on supercritical n-decane heat transfer. The overall average surface heat transfer coefficient could be even up to 27.5% higher than for an ordinary horizontal tube. It is indicated that more attention should be paid to the external factors when investigating supercritical flow and heat transfer in the research and development of scramjet engine cooling.</p>}},
  author       = {{Chen, Youqian and Li, Yong and Liu, Dechao and Sunden, Bengt and Xie, Gongnan}},
  issn         = {{1270-9638}},
  keywords     = {{Acceleration; Buoyancy; External factors; Heat transfer coefficient; Supercritical n-decane}},
  language     = {{eng}},
  publisher    = {{Elsevier Masson SAS}},
  series       = {{Aerospace Science and Technology}},
  title        = {{Influences of accelerating states on supercritical n-decane heat transfer in a horizontal tube applied for scramjet engine cooling}},
  url          = {{http://dx.doi.org/10.1016/j.ast.2020.106424}},
  doi          = {{10.1016/j.ast.2020.106424}},
  volume       = {{109}},
  year         = {{2021}},
}