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University of Oxford T6 Piston Reflected Shock Tunnel

University of Oxford / NWTF

University of Oxford, Oxford, England

Access: Yes

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Testing capabilities

  • Aerodynamics and aerothermal testing

Services

Hypersonic, reflected-shock, expansion-tunnel and shock-tube aerodynamic testing; boundary-layer stability, hypersonic intake, supersonic combustion and free-flight studies; high-speed optical and pressure/heat-transfer diagnostics.

Equipment

0.9 m x 0.9 m x 1.2 m test section; Mach 6–8; up to 8 km/s; up to 75 MPa and 5,000 K; up to 3 ms run time; remote model support, up to 128-channel 2 MHz DAQ, high-speed Schlieren, pressure transducers and thin-film heat-transfer gauges.

Standards

No accreditation or test standards stated on the cited facility page; profile explicitly says available to industry and academic users through NWTF.

Contact

Email: admin@nwtf.ac.uk

Approximate location

Oxford · Town location

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Sources