Henry R Hunczak

Starting and Operating Limits of Two Supersonic Wind Tunnels Utilizing Auxiliary Air Injection Downstream of the Test Section

Henry R Hunczak, Morris D Rousso, 1954 .

Characteristics of perforated diffusers at free-stream Mach number 1.90

Emil J Kremzier, Henry R Hunczak, 1950 .

Investigation at Mach Numbers 2.98 and 2.18 of Axially Symmetric Free-jet Diffusion with a Ram-jet Engine

Henry R Hunczak, 1952 .