Experimental investigations of scramjet combustor characteristics

T Scheuermann, J Chun… - 15th AIAA International …, 2008 - arc.aiaa.org
Future space transport vehilce or even aircraft are supposed to use airbreathing propulsion
systems for their flight in a wide range of hypersonic Mach numbers. The great benefit of …

Numerical investigation of a hydrogen-fueled scramjet combustor at flight conditions

E Rabadan, B Weigand - Progress in Propulsion Physics, 2013 - eucass-proceedings.eu
Numerical investigations of a hydrogen-fueled scramjet combustor at cruise flight conditions
of Mach 8 at an altitude of 30 km have been performed. Two combustor configurations were …

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 …

Analysis of a two-staged supersonic combustion chamber using experiments and simulations

J Vellaramkalayil, T Scheuermann… - 17th AIAA International …, 2011 - arc.aiaa.org
Future space transport vehicles or even aircrafts are supposed to use airbreathing
propulsion systems for their flight in a wide range of hypersonic Mach numbers. The great …

One-dimensional modelling of a scramjet combustor reacting flow

T Scheuermann, J Chun… - 15th AIAA International …, 2008 - arc.aiaa.org
Future hypersonic transport vehicles are supposed to use scramjet propulsion systems
instead of rocket based engines. The great advantage of a Scramjet engine is the higher …

Preliminary analysis of scramjet engines based on engineering models

TC Rolim, PGP Toro - Aerospace Science and Technology, 2015 - Elsevier
A mathematical model for analyzing two-dimensional scramjets was developed. The inlet
was modeled with the oblique shockwave relationships. The combustor and nozzle were …

Performance of a scramjet combustor with combined normal and tangential fuel injection

SA Rowan, A Paull - Journal of Propulsion and Power, 2006 - arc.aiaa.org
SUPERSONIC combustion ramjets, or scramjets, are expected to allow the economical
launch of satellites into low Earth orbit, cut travel times between major cities to a matter of …

Experimental and numerical study of a supersonic combustion chamber with different two-staged injection concepts

J Vellaramkalayil, T Scheuermann, S Winkler… - 46th AIAA/ASME/SAE …, 2010 - arc.aiaa.org
Future space transport vehicles or even high speed aircrafts are supposed to use air
breathing propulsion systems for their flight in a wide range of hypersonic Mach numbers …

Combustion Regimes in Inlet-fulled, Low Compression Scramjets

R Gehre, V Wheatley, R Boyce - 20th AIAA International Space Planes …, 2015 - arc.aiaa.org
In the 1950s and 60s, the concept of supersonic ramjet (scramjet) propulsion was introduced
by Weber & McKay1 and Billig. 2 For certain applications, this novel concept has a major …

A review of the scramjet experimental data base

RK Seleznev, ST Surzhikov, JS Shang - Progress in Aerospace Sciences, 2019 - Elsevier
The frontier in hypersonic flights via an air-breathing scramjet faces a formidable challenge,
because the operational principle is built on thermal compression, which is inherently …