Donald B. Smeltzer

Top-mounted inlet performance for a V/STOL fighter/attack aircraft configuration

Donald B. Smeltzer, 1987 .

Performance estimates for a supersonic axisymmetric inlet system.

Norman E. Sorensen, Donald B. Smeltzer, 1972 .

Variable Geometry for Supersonic Mixed-Compression Inlets

Norman E. Sorensen, Eldon A. Latham, Donald B. Smeltzer, 1976 .

Advanced supersonic inlet technology.

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

Test results at transonic speeds on a contoured over-the-wing propfan model

Donald B. Smeltzer, Ronald C. Smith, Alan D. Levin, 1986 .

Study of two axisymmetric inlets designed for Mach 3.5

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

Study of Two Axisymmetric Inlets Designed for Mach 3.5

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