D. Smeltzer

Study of two axisymmetric inlets designed for Mach 3.5

Norman E. Sorensen, Donald B. Smeltzer, N. Sorensen, 1976 .

Variable geometry for supersonic mixed-compression inlets

N. Sorensen, D. Smeltzer, E. Latham, 1974 .

Investigation of a mixed compression axisymmetric inlet at Mach number 5.3

D. Smeltzer, E. Latham, N. Sorenson, 1972 .

Advanced supersonic inlet technology.

Norman E. Sorensen, Eldon A. Latham, Donald B. Smeltzer, 1973 .