Magnetic field control of high-enthalpy shock wave/boundary-layer interactions using a fully implicit thermochemical non-equilibrium solver
H Jiang, J Liu, X Che, Y Du, W Huang, F Ding… - Aerospace Science and …, 2023 - Elsevier
Magnetohydrodynamic (MHD) heat shield systems have been proven to be highly effective
in hypersonic blunt-nosed bodies. Thus, it is natural to consider the application of MHD to …
in hypersonic blunt-nosed bodies. Thus, it is natural to consider the application of MHD to …
State-specific study of air in the expansion tunnel nozzle and test section
Thermochemical nonequilibrium in expansion tunnel nozzles is investigated numerically
using a state-to-state description in one dimension for representative air conditions. Limiting …
using a state-to-state description in one dimension for representative air conditions. Limiting …
Improved test time evaluation in an expansion tube
Traditionally, expansion tube test times have been experimentally evaluated using test
section mounted impact pressure probes. This paper proposes two new methods which can …
section mounted impact pressure probes. This paper proposes two new methods which can …
Development of a fast-response diamond calorimeter heat transfer gauge
RTP Geraets, M McGilvray, LJ Doherty… - … of Thermophysics and …, 2020 - arc.aiaa.org
A robust fast-response calorimeter heat transfer gauge called the Diamond Heat Transfer
Gauge has been developed for use in transient hypersonic ground test facilities. Gauges …
Gauge has been developed for use in transient hypersonic ground test facilities. Gauges …
Experimental and computational fluid dynamics study of Hayabusa reentry peak heating
EJ Fahy, DR Buttsworth, RJ Gollan… - Journal of Spacecraft …, 2021 - arc.aiaa.org
In this work, near-infrared and ultraviolet spectroscopic data collected during the Hayabusa
spacecraft reentry is used as the basis for validating numerical and experimental studies …
spacecraft reentry is used as the basis for validating numerical and experimental studies …
Experimental results of the electron transpiration cooling effect in the X2 expansion tunnel
OL Paxton, H Porat, IH Jahn - AIAA AVIATION 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-3808. vid Electron Transpiration
Cooling (ETC) is a novel heat transfer mechanism that could be used to manage the …
Cooling (ETC) is a novel heat transfer mechanism that could be used to manage the …
Scaled Apollo capsule heat flux measurements in the X3 expansion tube
CM James, R Ravichandran, DR Smith… - AIAA Aviation 2020 …, 2020 - arc.aiaa.org
Planetary entry thermal protection systems are a critical and mission limiting technology for
space exploration. Of special importance for super orbital Earth return, are the high velocity …
space exploration. Of special importance for super orbital Earth return, are the high velocity …
On the development of ETC test conditions in the X2 expansion tube
OL Paxton, H Porat, I Jahn - ASCEND 2021, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-4140. vid Electron Transpiration
Cooling (ETC) has been proposed as a mechanism to augment heat rejection from hot …
Cooling (ETC) has been proposed as a mechanism to augment heat rejection from hot …
Generating high-speed earth reentry test conditions in an expansion tube
Future space missions, such as return from Mars, will require entry speeds of the order of 15
km/s. These harsh conditions are dominated by radiative heat flux and have large modeling …
km/s. These harsh conditions are dominated by radiative heat flux and have large modeling …
[PDF][PDF] Flow characterization and modeling of the X2 and X3 expansion tubes
Abstract The Centre for Hypersonics at The University of Queensland operates the X2 and
X3 free-piston driven expansion tubes, which were designed primarily to study superorbital …
X3 free-piston driven expansion tubes, which were designed primarily to study superorbital …