T. G. Ayers

发表

Historical background and design evolution of the transonic aircraft technology supercritical wing

T. G. Ayers, J. B. Hallissy, T. Ayers, 1981 .

Effect of wing-transition location and slotted and unslotted flaps on aerodynamic characteristics of a fighter model at high subsonic speeds. [conducted in langley 8-foot transonic pressure tunnel

T. G. Ayers, 1969 .

Review of the 1980 Wind-Tunnel/Flight Correlation Panel

T. G. Ayers, 1982 .

The need for a hypersonic demonstrator

T. G. Ayers, 1990 .

A Wind-Tunnel Investigation of the Application of the NASA Supercritical Airfoil to a Variable-Wing-Sweep Fighter Airplane

T. G. Ayers, T. Ayers, 1973 .

Transonic wind-tunnel investigation of the maneuver potential of the NASA supercritical wing concept, phase 1

T. G. Ayers, J. B. Hallissy, 1977 .

Application of advanced aerodynamics to future transport aircraft

T. G. Ayers, A. L. Braslow, 1971 .

Supercritical aerodynamics - Worthwhile over a range of speeds.

T. G. Ayers, T. Ayers, 1972 .

NACA/NASA supersonic flight research

T. G. Ayers, 1990 .

Automated Water Control in Southern Alberta

T. G. Ayers, B. C. Palmer, 1987 .

A review of flight-to-wind tunnel drag correlation

T. G. Ayers, E. J. Saltzman, 1981 .