D. W. Bartlett

发表

The NASA supercritical-wing technology

D. W. Bartlett, J. C. Patterson, 1978 .

Wind-tunnel development of underwing leading-edge vortex generators on a NASA supercritical-wing research airplane configuration

T. C. Kelly, D. W. Bartlett, C. D. Harris, 1973 .

Tabulated pressure measurements of a NASA supercritical-wing research airplane model with and without fuselage area-rule additions at Mach 0.25 to 1.00

D. W. Bartlett, C. D. Harris, D. W. Bartlett, 1972 .

Effects of landing gear, speed brake and protuberances on the longitudinal aerodynamic characteristics of an NASA supercritical-wing research airplane model

D. W. Bartlett, G. Sangiorgio, 1975 .

Energy Efficient Transport - Technology in hand

D. W. Bartlett, D. B. Middleton, R. V. Hood, 1984 .

Wind-tunnel investigation of basic aerodynamic characteristics of a supercritical-wing research airplane configuration

R. J. Re, D. W. Bartlett, 1972 .

Effects of differential and symmetrical aileron deflection on the aerodynamic characteristics of an NASA supercritical-wing research airplane model

D. W. Bartlett, 1975 .

Energy efficient transport technology: Program summary and bibliography

D. W. Bartlett, D. B. Middleton, R. V. Hood, 1985 .

Tabulated pressure measurements on an executive-type jet transport model with a supercritical wing

D. W. Bartlett, 1975 .

Laminar Flow Flight Experiments — A Review

F. S. Collier, D. W. Bartlett, D. V. Maddalon, 1992 .

Aerodynamic characteristics of an NASA supercritical-wing research airplane model with and without fuselage area-rule additions at Mach 0.25 to 1.00

D. W. Bartlett, C. D. Harris, 1972 .