Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties

CM James, DE Gildfind, SW Lewis, RG Morgan… - Shock Waves, 2018 - Springer
Expansion tubes are an important type of test facility for the study of planetary entry flow-
fields, being the only type of impulse facility capable of simulating the aerothermodynamics …

Vacuum ultraviolet spectral measurements for superorbital earth entry in X2 expansion tube

UA Sheikh, RG Morgan, TJ McIntyre - Aiaa Journal, 2015 - arc.aiaa.org
Experiments were conducted using the X2 expansion tube at two conditions representative
of flight velocities of 10.0 and 12.2 km/s for a vehicle entry into Earth's atmosphere …

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 …

Free-piston driver performance characterisation using experimental shock speeds through helium

DE Gildfind, CM James, RG Morgan - Shock Waves, 2015 - Springer
Tuned free-piston driver operation involves configuring the driver to produce a relatively
steady blast of driver gas over the critical time scales of the experiment. For the purposes of …

T6: The Oxford University Stalker Tunnel

M McGilvray, LJ Doherty, RG Morgan… - 20th AIAA International …, 2015 - arc.aiaa.org
The University of Oxford has embarked on developing the UKs fastest wind tunnel, T6, in
collaboration with the University of Queensland (Australia) using technology pioneered by …

[PDF][PDF] Superorbital re-entry shock layers: flight and laboratory comparisons

EJ Fahy - 2017 - core.ac.uk
Hypervelocity re-entry through the Earth's atmosphere surrounds an aeroshell with a
radiating shock layer, which has complex and potentially critical interactions with the thermal …

Quantitative emission spectroscopy for superorbital reentry in expansion tube X2

T Hermann, S Löhle, U Bauder, R Morgan… - … of Thermophysics and …, 2017 - arc.aiaa.org
A superorbital reentry flow was realized in the X2 expansion tunnel of the Centre for
Hypersonics of the University of Queensland, resulting in measurements of electronic …

[PDF][PDF] Radiation from simulated atmospheric entry into the gas giants

C James, RG Morgan - 18th Australasian Fluid Mechanics …, 2018 - flair.monash.edu.au
When entering a gas giant, the heat transfer to the surface of the entry vehicle is primarily
driven by radiation from the shock layer. It is not currently known how existing techniques …

Optical thickness measurements of vacuum ultraviolet radiation in the X2 expansion tube

UA Sheikh, RG Morgan, TJ McIntyre - Aiaa Journal, 2016 - arc.aiaa.org
Experiments were conducted in the X2 expansion tube to measure vacuum ultraviolet
radiation from shock layers representative of reentry conditions at flight equivalent velocities …

Condition development and commissioning of the Oxford T6 Stalker Tunnel in reflected shock tunnel mode

S Subiah, P Collen, L Doherty, R Penty Geraets… - 2019 - ora.ox.ac.uk
To provide data for the design of re-entry vehicles and validation of computational models,
ground testing facilities such as the Oxford T6 Stalker Tunnel are crucial. The current work …