Surface pressure measurements on a free-flying cone at mach 7 using pressure sensitive paint by Wheeler, C, Hyslop, A, Vieira, J, Le Page, L, Quinn, MK, Chowdhury, N, Doherty, L

“…The model also featured an on-board inertial measurement unit, thereby providing simultaneous measurement of the aerodynamic forces and surface pressure distribution. The measured surface pressure was compared with analytical and numerical predictions and found to be ≈3kPa higher than expected.…”

Mixing characteristics in a hypersonic flow around a transpiration cooled flat plate model by Hermann, T, Ifti, H, McGilvray, M, Doherty, L, Geraets, R

“…A flat plate model is used which is equipped with a gas injection system, four surface mounted heat flux gauges and three surface pressure sensors located downstream of the injection point. …”

Commissioning of the Oxford High Density Tunnel (HDT) for boundary layer stability measurements at Mach 7 by Wylie, S, Doherty, L, McGilvray, M

“…Analysis of high-frequency surface pressure fluctuations at various azimuthal angles and angles of attack up to 12 degrees have shown good agreement with the H2K results, verifying that the HDT can be used for boundary layer instability measurements.…”

Mixing Characteristics in a Hypersonic Flow around a Transpiration Cooled Flat Plate Model - Dataset by Hermann, T, Ifti, H S, McGilvray, M, Doherty, L, Penty Geraets, R

“…A flat plate model is used which is equipped with a gas injection system, four surface mounted heat flux gauges and three surface pressure sensors located downstream of the injection point. …”