Results 161 to 170 of about 9,113 (233)
Influence of injection angles on flow structures and mixing properties in a supersonic combustor at low Mach supersonic crossflow. [PDF]
Sci RepZhang L +4 more
europepmc +1 more source
Low-cost open-source camera view splitter (quadscope) for flow diagnostics. [PDF]
HardwareXSahoo A, DeBoskey RD, Narayanaswamy V.
europepmc +1 more source
Hydrogen Atom Abstraction Reaction from Silane with Hydrogen and Methyl Radicals: Rate Constants and Kinetic Isotopic Effects. [PDF]
J Phys Chem AKano FG +4 more
europepmc +1 more source
Mitigating hypersonic heat barrier via direct cooling enhanced by leidenfrost inhibition. [PDF]
Nat CommunWang JX +6 more
europepmc +1 more source
CFD-based optimization and experimental validation of supersonic separator design with angular injection swirler for efficient gas dehydration. [PDF]
Sci RepShoghl SN +3 more
europepmc +1 more source
Some of the next articles are maybe not open access.
Related searches:
Related searches:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009
An investigation is undertaken into the potential use of carbon-carbon materials for Scramjet combustors and configurations utilising regenerative and radiative cooling are considered. The analysis uses the ANSYS package to couple a CFD analysis of the fuel cooling with a structural thermal analysis.
Zander, Fabian, Morgan, Richard
openaire +2 more sources
An investigation is undertaken into the potential use of carbon-carbon materials for Scramjet combustors and configurations utilising regenerative and radiative cooling are considered. The analysis uses the ANSYS package to couple a CFD analysis of the fuel cooling with a structural thermal analysis.
Zander, Fabian, Morgan, Richard
openaire +2 more sources
Noise Generated in a Scramjet Combustor
AIAA SCITECH 2023 Forum, 2023This paper presents the noise levels generated inside a two-dimensional scramjet combustor at Mach 7.3 freestream using the focused laser differential interferometric (FLDI) technique. FLDI measurements were taken at the front, middle, and rear of the combustor’s center plane under unfueled, combustion-suppressed, and combustion-on conditions ...
Ramprakash Ananthapadmanaban +3 more
openaire +3 more sources
2007
This paper outlines the theory of radical farming in scramjets and describes the experimental scramjet model that was designed to investigate it. Experiments were conducted at two conditions; a 3MJ/kg condition corresponding to Mach 7.9 flight at an altitude of 24km and a 4MJ/kg condition corresponding to Mach 9.1 flight at an altitude of 32km.
Odaml J., Paull A.
openaire +2 more sources
This paper outlines the theory of radical farming in scramjets and describes the experimental scramjet model that was designed to investigate it. Experiments were conducted at two conditions; a 3MJ/kg condition corresponding to Mach 7.9 flight at an altitude of 24km and a 4MJ/kg condition corresponding to Mach 9.1 flight at an altitude of 32km.
Odaml J., Paull A.
openaire +2 more sources