A New Method of Thermal Protection by Opposing Jet for a Hypersonic Aeroheating Strut

This paper presents the numerical investigation of thermal protection of scramjet strut by opposing jet in supersonic stream of Mach number 6 with a hydrogen fueled scramjet strut model using CFD software. Simulation results indicate that when a small amount of fuel is injected from the nose of the...

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Veröffentlicht in:	Journal of thermal science 2017-06, Vol.26 (3), p.282-288
Hauptverfasser:	Qin, Jiang, Ning, Dongpo, Feng, Yu, Zhang, Junlong, Feng, Shuo, Bao, Wen
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic heating Classical and Continuum Physics Computer simulation Drag Engineering Fluid Dynamics Engineering Thermodynamics Enthalpy Heat and Mass Transfer Heat flux Mach number Mathematical models Nose Physics Physics and Astronomy Pressure ratio Supersonic aircraft Thermal protection
Online-Zugang:	Volltext
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