Numerical Simulation of Transpiration Cooling for a High-Speed Vehicle with Substructure-Reference-Cited by-同舟云学术

Numerical Simulation of Transpiration Cooling for a High-Speed Vehicle with Substructure

Published:2021-03-01 Issue: Volume: Page:1-12
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Naved Imran¹^ORCID,Hermann Tobias¹,McGilvray Matthew¹

Affiliation:

1. University of Oxford, Oxford, England OX2 0ES, United Kingdom

Funder

Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference18 articles.

1. SchweikertS.HaldH. “Characterization of Actively Cooled Porous C/C Wall Segments According to Pressure Loss and Internal Temperature Distribution,” Tech. Rept. 2013, https://elib.dlr.de/86614/.

2. Heat pipe and surface mass transfer cooling of hypersonic vehicle structures

3. Surface cooling of scramjet engine inlets using heat pipe, transpiration, and film cooling

4. EdneyB. “Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speeds in the Presence of an Impinging Shock,” Aeronautical Research Inst. of Sweden TR FFA-115, Stockholm, 1968, https://www.osti.gov/biblio/4480948-anomalous-heat-transfer-pressure-distributions-blunt-bodies-hypersonic-speeds-presence-impinging-shock [retrieved 19 June 2020].

5. Effects of shock impingement on the heat transfer around blunt bodies.

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