Injectant Molecular Weight Effects in Injectors for Circular Scramjet Combustors

C Rock, J Schetz, R Ungewitter - 48th AIAA Aerospace Sciences …, 2010 - arc.aiaa.org
In view of the very high freestream velocity of scramjets reaching Mach 10, fuel residence
time is on the order of milliseconds1 and supersonic combustion presents a challenge in …

Experimental and numerical studies of a strut injector for round scramjet combustors

C Rock, J Schetz, R Ungewitter - 16th AIAA/DLR/DGLR International …, 2009 - arc.aiaa.org
In view of the very high freestream velocity of scramjets reaching Mach 10, fuel residence
time is on the order of milliseconds1 and supersonic combustion presents a challenge in …

Flush-wall, diamond-shaped fuel injector for high Mach number scramjets

PM Grossman, L Maddalena, JA Schetz - Journal of Propulsion and …, 2008 - arc.aiaa.org
BECAUSE to the of very high freestream velocity of scramjets reaching Mach 10, fuel
residence time is on the order of milliseconds [1], and supersonic combustion presents an …

Wall injectors for high Mach number scramjets

P Grossman, L Maddalena, J Schetz - 42nd AIAA/ASME/SAE/ASEE …, 2006 - arc.aiaa.org
UE to the short fuel residence time inside a scramjet (on the order of milliseconds)
supersonic combustion forms an interesting challenge. Enhanced penetration and mixing …

Complex wall injector array for scramjet combustors

J Schetz, L Maddalena, R Throckmorton… - 46th AIAA Aerospace …, 2008 - arc.aiaa.org
As a result of the very high freestream velocity of scramjets reaching Mach 10, fuel residence
time is on the order of milliseconds, 1 and efficient supersonic combustion presents a …

Improved aerodynamic-ramp injector in supersonic flow

LS Jacobsen, SD Gallimore, JA Schetz… - Journal of Propulsion …, 2003 - arc.aiaa.org
IN a scramjet engine, not only must the injected fuel mix quickly into the surrounding
freestream, the process must also induce the lowest aerothermodynamiclosses possible …

Experimental investigation of a swept-strut fuel-injector concept for scramjet application

GY Anderson, PG Reagon, PB Gooderum, WR Russin - 1977 - ntrs.nasa.gov
Results are presented of an experiment to investigate the behavior at Mach 4 flight
conditions of the swept-strut fuel-injector concept employed in the Langley integrated …

Fuel/air mixing characteristics of strut injections for scramjet combustor applications

CJ Tam, KY Hsu, M Gruber, C Raffoul - 26th AIAA Applied …, 2008 - arc.aiaa.org
One of the principal challenges in developing large-scale scramjet-engine designs is the
fuel-injection strategy, ie., the penetration and mixing of the fuel in the combustor. Injector …

Evaluation of parallel injector configurations for Mach 2 combustion

GB Northam, I Greenberg, CS Byington… - Journal of Propulsion …, 1992 - arc.aiaa.org
EXPERIMENTAL and theoretical studies are being con-ducted to explore techniques to
enhance mixing for scramjet combustion. 1 The Hypersonic Propulsion Branch at NASA's …

Experimental assessment of a fuel injector for scramjet applications

T Mathur, S Cox-Stouffer, KY Hsu, J Crafton… - 36th AIAA/ASME/SAE …, 2000 - arc.aiaa.org
Fuel injection and mixing have been identified by the Air Force Hypersonic Technology
Office1 as significant" technological challenges" that must be addressed as a prerequisite …