Numerical investigation of scramjet strut injector cooling for different fuel mass fluxes and strut material properties at mach 8 flight conditions

P Gerlinger, YH Simsont - Acta Astronautica, 2019 - Elsevier
The thermal load on a lobed scramjet (supersonic combustion ramjet) strut injector is
investigated numerically for Mach 8 flight conditions. For this purpose, coupled 3D RANS …
被引用次数：30 相关文章

Numerical investigation of scramjet strut injector cooling for different fuel mass fluxes and strut material properties at mach 8 flight conditions

P Gerlinger, YH Simsont - Acta Astronautica, 2019 - ui.adsabs.harvard.edu
The thermal load on a lobed scramjet (supersonic combustion ramjet) strut injector is
investigated numerically for Mach 8 flight conditions. For this purpose, coupled 3D RANS …
[PDF] dlr.de

[PDF][PDF] Numerical investigation of scramjet strut injector cooling for different fuel mass fluxes and strut material properties at Mach 8 flight conditions

P Gerlinger, YH Simsont - Acta Astronautica, 2019 - elib.dlr.de
The thermal load on a lobed scramjet (supersonic combustion ramjet) strut injector is
investigated numerically for Mach 8 flight conditions. For this purpose, coupled 3D RANS …
[PDF] core.ac.uk

[PDF][PDF] Numerical investigation of scramjet strut injector cooling for different fuel mass fluxes and strut material properties at Mach 8 flight conditions

P Gerlinger, YH Simsont - core.ac.uk
The thermal load on a lobed scramjet (supersonic combustion ramjet) strut injector is
investigated numerically for Mach 8 flight conditions. For this purpose, coupled 3D RANS …