F.-J. CHEN

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

I. E. Beckwith, T. R. Creel, F.-J. CHEN et al. · 21st Aerospace Sciences Meeting · 1983 · 60 citations

Engineering, Aerospace Engineering, Physics +16

Instabilities and transition in the wall boundary layers of low-disturbance supersonic nozzles

F.-J. CHEN, I. E. Beckwith · 1985 · 39 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

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

I. E. Beckwith, F.-J. CHEN, T. R. Creel · 1986 · 35 citations

Engineering, Aerospace Engineering, Physics +17

Design and fabrication requirements for low noise supersonic/hypersonic wind tunnels

F.-J. CHEN · NASA STI Repository (National Aeronautics and Space Administration) · 34 citations

Engineering, Aerospace Engineering, Acoustics +16

Design and operational features of low-disturbance wind tunnels at NASA Langley for Mach numbers from 3.5 to 18

I. E. Beckwith, F.-J. CHEN, Stephen Wilkinson et al. · 1990 · 32 citations

Engineering, Aerospace Engineering, Mechanical Engineering +12