Performance capability experiments in T6: A hypervelocity, transient and multi-mode ground test facility for high-enthalpy aerothermodynamics research

Performance capability experiments in T6: A hypervelocity, transient and multi-mode ground test facility for high-enthalpy aerothermodynamics research

Bibliographic Details
Main Authors:	Collen, P, Doherty, L, Subiah, S, Hyslop, A, McGilvray, M
Format:	Conference item
Published:	ESA Conference Bureau 2019

Similar Items

Measurements of radiating hypervelocity air shock layers in the T6 free-piston driven shock tube
by: Collen, P, et al.
Published: (2019)

Condition development and commissioning of the Oxford T6 Stalker Tunnel in reflected shock tunnel mode
by: Subiah, S, et al.
Published: (2019)

CONDITION DEVELOPMENT AND COMMISSIONING OF THE OXFORD T6 STALKER TUNNEL IN REFLECTED SHOCK TUNNEL MODE - Dataset
by: Hermann, T, et al.
Published: (2022)

Integration of arc-jet in impulse facility for hypervelocity aerothermal testing with ablation
by: Chang, EWK, et al.
Published: (2023)

Assessment of high enthalpy flow conditions for re-entry aerothermodynamics in the plasma wind tunnel facilities at IRS
by: Loehle, S, et al.
Published: (2021)

Measurement of the aerothermodynamic state in a high enthalpy plasma wind-tunnel flow
by: Hermann, T, et al.
Published: (2017)

Measurement of aeroheating of satellite components at true flight total enthalpies
by: Leader, J, et al.
Published: (2022)

Development of a high-enthalpy ground test facility for shock-layer radiation
by: Collen, PL
Published: (2021)

Aerodynamic design of nozzles with uniform outflow for hypervelocity ground-test facilities
by: Chan, W, et al.
Published: (2018)

Comparison of force measurement techniques in a short duration hypersonic facility
by: Hyslop, A, et al.
Published: (2024)

Boundary layer instabilities in high and low enthalpy hypersonic facilities using high speed schlieren
by: Subiah, SD
Published: (2022)

Basics of aerothermodynamics /
by: 453305 Hirschel, Ernst Heinrich
Published: (2004)

Development of combined hypersonic test facility for aerothermodynamic testing
by: Sungmo Yang, et al.
Published: (2024-01-01)

Simulation of a low enthalpy ablator into a hypersonic boundary-layer
by: Condren, WJ, et al.
Published: (2024)

The Oxford T6 Stalker tunnel: performance, upgrades and new modes of operation
by: McGilvray, M, et al.
Published: (2022)

Effects of ultrafast laser energy deposition on a hypervelocity boundary layer
by: Le Page, L, et al.
Published: (2024)

Absolute measurements of air shock-layer radiation in the T6 Aluminium Shock Tube
by: Collen, PL, et al.
Published: (2023)

Hypersonic boundary layer instability measurements at Mach 7 and flight total enthalpy
by: Wylie, S, et al.
Published: (2019)

Aerothermodynamic test instrumentation and measurement
by: Society of Automotive Engineers (United States)
Published: (1989)

Aerothermodynamics of aircraft engine components/
by: Oates, Gordon C.
Published: (1985)

Modelling the complete operation of a free-piston shock tunnel for a low enthalpy condition
by: McGilvray, M, et al.
Published: (2013)

Modelling the complete operation of a free-piston shock tunnel for a low enthalpy condition
by: McGilvray, M, et al.
Published: (2013)

Development and commissioning of the T6 Stalker Tunnel
by: Collen, P, et al.
Published: (2021)

Free-flight aerodynamic testing of a 7 degree half-angle cone
by: Hyslop, A, et al.
Published: (2021)

Aerothermodynamics of gas turbine and rocket propulsion /
by: 176253 Oates, Gordon C.
Published: (1988)

Aerothermodynamics of gas turbine and rocket propulsion /
by: 176253 Oates, Gordon C.
Published: (1984)

Aerothermodynamics of gas turbine and rocket propulsion /
by: 176253 Oates, Gordon C.
Published: (1997)

Ground effects on the hypervelocity jet flow and the stability of projectile
by: Zijie Li, et al.
Published: (2018-01-01)

Aerothermodynamics in combustors: IUTAM symposium, Taipei, Taiwan 1991 /
by: Lee R. S. L., et al.
Published: (1992)

Aerothermodynamic Optimization of Aerospace Plane Airfoil Leading Edge
by: Chen Zhou, et al.
Published: (2017-10-01)

Hypervelocity Gouging Impacts /
by: Cinnamon, John D., author 520482
Published: (2009)

Commissioning of the T6 Stalker Tunnel
by: Collen, P, et al.
Published: (2019)

Aerothermodynamics and operation of turbine system under unsteady pulsating flow
by: Lee, Jinwook, Ph. D. Massachusetts Institute of Technology
Published: (2015)

Commissioning of upgrades to T6 to study giant planet entry
by: Steer, J, et al.
Published: (2024)

Commissioning Ludwieg mode with isentropic compression heating for the Oxford High Density Tunnel
by: Ivison, W, et al.
Published: (2024)

Design of Hypervelocity-Impact Damage Evaluation Technique Based on Bayesian Classifier of Transient Temperature Attributes
by: Haonan Zhang, et al.
Published: (2020-01-01)

Aerothermodynamic Shape Optimization for Re-entry Capsule Using Genetic Algorithms
by: Ionut BUNESCU, et al.
Published: (2019-12-01)

The fidelity of DSMC method to analyze the aerothermodynamics of the pure continuum flow regime
by: Md. Zahid Hasan
Published: (2020-11-01)

Analysis of ground distance effect on hypervelocity jet flow and stability of projectile in half-space
by: Zijie Li, et al.
Published: (2022-04-01)

Tool for rapid transient transpiration cooled re-entry simulation
by: Hermann, T, et al.
Published: (2019)