[PDF][PDF] Experimental investigation of different scramjet hydrogen injection systems

K Hannemann, JM Schramm, S Karl… - Proceedings of the 6th …, 2008 - researchgate.net
Supersonic combustion experiments of a complete scramjet configuration consisting of
intake, combustor and nozzle were performed in the High Enthalpy Shock Tunnel Göttingen …

Ground testing of the HyShot II scramjet configuration in HEG

J Martinez Schramm, S Karl, K Hannemann… - 15th AIAA International …, 2008 - arc.aiaa.org
Ground based testing of the HyShot II supersonic combustion ramjet flight configuration was
carried out in the High Enthalpy Shock Tunnel Göttingen, HEG, of the German Aerospace …

CFD analysis of the HyShot supersonic combustion flight experiment configuration

S Karl, K Hannemann, J Steelant, A Mack - 14th AIAA/AHI Space …, 2006 - arc.aiaa.org
Testing of the HyShot II scramjet configuration was carried out in the High Enthalpy Shock
Tunnel Goettingen, HEG, of the German Aerospace Center, DLR. Computational fluid …

CFD analysis of unstart characteristics of the HyShot-II scramjet configuration in the HEG shock tunnel

S Karl, J Martinez Schramm, K Hannemann… - 17th AIAA International …, 2011 - arc.aiaa.org
Ground based testing of the generic HyShot II scramjet configuration was carried out in the
High Enthalpy Shock Tunnel Göttingen, HEG, of the German Aerospace Center, DLR, and …

CFD analysis of the HyShot II scramjet experiments in the HEG shock tunnel

S Karl, K Hannemann, A Mack, J Steelant - 15th AIAA International …, 2008 - arc.aiaa.org
Testing of the HyShot II scramjet configuration was carried out in the High Enthalpy Shock
Tunnel Goettingen, HEG, of the German Aerospace Center, DLR. Computational fluid …

HyShot scramjet testing in the HEG

AD Gardner - 2007 - osti.gov
A study of the suitability of ground-based facilities for simulating the flow and combustion in
scramjets has been carried out. A 1: 1 scale wind tunnel model was developed for the HEG …

Cfd analysis of unsteady combustion phenomena in the hyshot-ii scramjet configuration

S Karl, S Laurence, J Martinez Schramm… - 18th AIAA/3AF …, 2012 - arc.aiaa.org
Ground based testing of the generic HyShot II scramjet configuration was carried out in the
High Enthalpy Shock Tunnel Göttingen, HEG, of the German Aerospace Center, DLR, and …

Mach 8 ground tests of the hypermixer scramjet for HyShot-IV flight experiment

T Sunami, K Itoh, K Satoh, T Komuro - 14th AIAA/AHI Space Planes and …, 2006 - arc.aiaa.org
A hydrogen fueled scramjet engine with a wall-mounted hypermixer injector is examined at
a Mach 8 flight condition in the high enthalpy shock tunnel. The hypermixer, which is …

Ground testing of the HyShot supersonic combustion flight experiment in HEG and comparison with flight data

A Gardner, J Steelant, A Paull… - 40th AIAA/ASME/SAE …, 2004 - arc.aiaa.org
The first phase of the HyShot supersonic combustion ramjet (scramjet) flight experiment
program of The University of Queensland in Australia was designed to provide benchmark …

Numerical and experimental investigation of a two-staged supersonic combustion chamber

J Vellaramkalayil, T Scheuermann… - 16th AIAA/DLR/DGLR …, 2009 - arc.aiaa.org
I. Introduction uture space transport vehicles or even aircrafts are supposed to use air
breathing propulsion systems for their flight in a wide range of hypersonic Mach numbers …