S. L. Treon

On the use of freon-12 for increasing Reynolds number in wind-tunnel testing of three dimensional aircraft models at subcritical and supercritical Mach numbers

F. T. Abbott, S. L. Treon, W. R. Hofstetter, 1971 .

Data correlation from investigations of a high- subsonic speed transport aircraft model in three major transonic wind tunnels.

S. L. Treon, W. R. Hofstetter, J. R. Hagerman, 1969 .

Further correlation of data from investigations of a high-subsonic-speed transport aircraft model in three major transonic wind tunnels

S. L. Treon, J. R. Hagerman, F. W. Steinle, 1971 .

U.S. aerospace industry opinion of the effect of computer-aided prediction-design technology on future wind-tunnel test requirements for aircraft development programs

S. L. Treon, 1979 .