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Mach 10 Computational Study of a Three-Dimensional Scramjet Inlet Flow Field

open access: yes, 1995
The present work documents the computational results for a combined computational and experimental parametric study of the internal aerodynamics of a generic three-dimensional sidewall-compression scramjet inlet configuration at Mach 10.
Scott D. Holland
core  

Usage of serpentine injector for hydrogen mixing at combustion chamber of scramjet engine via a computational study. [PDF]

open access: yesSci Rep
Mir A   +7 more
europepmc   +1 more source

High fidelity simulations of unstart phenomena in a scramjet inlet due to angle of attack [PDF]

open access: yes
This work investigates the unsteady behavior of unstart phenomena within a scramjet inlet using advanced computational techniques. Scramjets and ramjets, with their reliance on inlet compression, offer promising airbreathing propulsion for hypersonic ...
Bravo, Luis   +4 more
core  

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