Edwin J. Saltzman

Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2

Edwin J. Saltzman, 1961 .

Transonic flight evaluation of the effects of fuselage extension and indentation on the drag of a 60-degree delta wing interceptor airplane

Edwin J. Saltzman, William P. Asher, 1957 .

Preliminary Full-Scale Power-Off Drag of the X-15 Airplane for Mach Numbers from 0.7 to 3.1

Edwin J. Saltzman, 1960 .

In-flight lift-drag characteristics for a forward-swept wing aircraft and comparisons with contemporary aircraft)

John W. Hicks, Edwin J. Saltzman, E. J. Saltzman, 1994 .