J. L. Thomas

SF system: Shore terminal facilities and fault location

R. L. Lynch, C. A. Von Roesgen, J. L. Thomas, 1970, Bell Syst. Tech. J..

Low-speed power effects on advanced fighter configurations with two-dimensional deflected thrust

L. P. Yip, J. W. Paulson, J. L. Thomas, 1977 .

Powered low-aspect-ratio Wing In Ground effect (WIG) aerodynamic characteristics. [conducted in Langley V/STOL tunnel

R. J. Margason, J. W. Paulson, J. L. Thomas, 1979 .

Effects of deflected thrust on the stability and performance characteristics of a close-coupled canard fighter configuration

L. P. Yip, J. W. Paulson, J. L. Thomas, 1977 .

Transition aerodynamics for close-coupled wing-canard configuration

M. M. Winston, J. W. Paulson, J. L. Thomas, 1979 .

Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations. [conducted in Langley C/STOL tunnel

J. W. Paulson, J. W. Paulson, J. L. Thomas, 1979 .