F. Chen

Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel

I. E. Beckwith, T. R. Creel, F. J. Chen, 1985 .

Design requirements for the NASA Langley supersonic low-disturbance wind tunnel

I. E. Beckwith, F. J. Chen, T. R. Creel, 1986 .

Free stream noise and transition measurements in a Mach 3.5 pilot quiet tunnel

I. E. Beckwith, T. R. Creel, J. Kendall, 1983 .