1. A transient flow facility for the study of the thermofluid-dynamics of a full stage turbine under engine representative conditions;Ainsworth,1988
2. A review of the AFRL turbine research facility;Anthony,2013
3. Design requirements for the NASA Langley supersonic low-disturbance wind tunnel;Beckwith,1986
4. Hypersonic wind-tunnel measurements of boundary-layer pressure fluctuations;Casper,2009
5. Design of the Purdue experimental turbine aerothermal laboratory for optical and surface aerothermal measurements;Paniagua;J. Eng. Gas Turbines Power,2019