Enhancing the test time performance of Ludwieg tunnels

Enhancing the test time performance of Ludwieg tunnels

Ground testing at hypersonic conditions requires either expensive heating or reduced test time. This paper discusses further developments to a mode of operation for Ludwieg Tunnels - Plenum Augmented Ludwieg Mode (PALM) - in the Oxford High Density Tunnel (HDT). PALM offers increased test time perfo...

書目詳細資料
Main Authors:	Hillyer, J, Doherty, L, Hambidge, C, McGilvray, M
格式:	Conference item
語言:	English
出版:	Aerospace Research Central 2024

相似書籍

Extension of test time in Ludwieg tunnels
由: Hillyer, J, et al.
出版: (2022)

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

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

Starting Process of a Double-Throat Ludwieg Tube Tunnel and the Extension of Its Effective Running Time
由: Chuangchuang LI, et al.
出版: (2024-01-01)

Flow Characterization of the UTSA Hypersonic Ludwieg Tube
由: Eugene N. A. Hoffman, et al.
出版: (2023-05-01)

Shock radiation tests for Ice Giant entry probes including CH4 in the T6 free-piston driven wind tunnel
由: Steer, J, et al.
出版: (2022)

Commissioning of the Oxford High Density Tunnel (HDT) for boundary layer stability measurements at Mach 7
由: Wylie, S, et al.
出版: (2018)

T6: The Oxford University Stalker Tunnel
由: McGilvray, M, et al.
出版: (2015)

T6: The Oxford University Stalker tunnel
由: McGilvray, M, et al.
出版: (2015)

Development of a novel mass flow measurement device for high speed inlet testing
由: Doherty, L, et al.
出版: (2019)

Experimental simulation of a Galileo sub-scale model at Ice Giant entry conditions in the T6 free-piston driven wind tunnel
由: Steer, J, et al.
出版: (2022)

The Oxford High Density Tunnel
由: McGilvray, M, et al.
出版: (2015)

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

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

Experimental performance evaluation of a streamline traced inlet at off-design conditions
由: Tyler, T, et al.
出版: (2024)

Thermal effects of plume impingement on a hypersonic vehicle
由: Hillyer, J, et al.
出版: (2022)

Refurbishment and characterisation of the Oxford Low Density Hypersonic Wind Tunnel
由: Donaldson, N, et al.
出版: (2019)

A method for direct shear measurement of large scale roughened surfaces in short duration hypersonic facilities
由: Steuer, D, et al.
出版: (2023)

Experimental studies of hypersonic shock impingement on a transpiration-cooled flat plate
由: Naved, I, et al.
出版: (2023)

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

Laminar transpiration cooling experiments in hypersonic flow
由: Ifti, HS, et al.
出版: (2022)

Performance capability experiments in T6: A hypervelocity, transient and multi-mode ground test facility for high-enthalpy aerothermodynamics research
由: Collen, P, et al.
出版: (2019)

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

Laminar transpiration cooling experiments in hypersonic flow - Dataset
由: Ifti, H S, et al.
出版: (2022)

Experimental investigation of the effect of steps and gaps on hypersonic vehicles
由: Ivison, W, et al.
出版: (2022)

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

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

Thermal-fluid-structural analysis of the Oxford High Density Tunnel
由: Neely, A, et al.
出版: (2014)

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

The combined effects of large-scale roughness and mass injection in hypersonic flow
由: Condren, WJ, et al.
出版: (2024)

A method for IR measurement of large scale roughened surfaces in hypersonic flow
由: Condren, W, et al.
出版: (2023)

Investigation of fluidic thrust vectoring for scramjets
由: Hambidge, C, et al.
出版: (2023)

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

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

LAPCAT II intake starting tests
由: McGilvray, M, et al.
出版: (2015)

Aerodynamic testing of the Skylon spaceplane
由: Hyslop, A, et al.
出版: (2019)

Quantifying the surface heat transfer on transpiration cooled porous materials in laminar and turbulent hypersonic boundary layers
由: Naved, I, et al.
出版: (2022)

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

Testing a transpiration cooled Zirconium-Di-Boride sample in the plasma tunnel at IRS
由: Ewenz Rocher, M, et al.
出版: (2019)

Stagnation point heat flux measurements in a plasma wind tunnel using a diamond heat transfer gauge
由: Penty Geraets, R, et al.
出版: (2019)