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A physical model for solving the dredging thermal protection system of hypersonic vehicle leading edge

The dredging thermal protection system is considered as a thermal protection method to prevent hypersonic vehicles whose leading edges work in the serious aerodynamic heating that seriously affects the performance and safety of the aircraft. This paper uses a special matrix splitting scheme and a hi...

Ausführliche Beschreibung

Gespeichert in:
Bibliografische Detailangaben
Hauptverfasser: Junjun Sun, Qingyong. Zhu
Format: Artigo
Sprache:Inglês
Veröffentlicht: AIP Publishing LLC 2019-02-01
Schriftenreihe:AIP Advances
Online-Zugang:http://dx.doi.org/10.1063/1.5083820
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