Jerome Pasamanick

Langley Full-Scale-Tunnel Investigation of the Fuselage Boundary Layer on a Typical Fighter Airplane with a Single Liquid-Cooled Engine

K. R. Czarnecki, Jerome Pasamanick, 1946 .

The Effect of Boundary-layer Control by Suction and Several High-lift Devices on the Longitudinal Aerodynamic Characteristics of a 47.5 Degree Sweptback Wing-fuselage Combination

Jerome Pasamanick, Anthony J Proterra, 1948 .

Langley full-scale-tunnel tests of the Custer Channel Wing airplane

Jerome Pasamanick, 1953 .