B. W. Sanders

Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-value controlled inlet stability bypass system when subjected to internal and external airflow transients

B. W. Sanders, B. Sanders, 1980 .

Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50

R. W. Cubbison, B. W. Sanders, B. Sanders, 1968 .

Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet. [Lewis 10- by 10-ft. supersonic wind tunnel test

B. W. Sanders, 1980 .