Search U.S. government technical reports digitized or harvested by TRAIL.
Effect of Propeller-Axis Angle of Attack on Thrust Distribution Over the Propeller Disk in Relation to Wake-Survey Measurement of Thrust
[Memorandums on the Subject of D-558 Airplane]
An Investigation of the Characteristics of Three NACA 1-Series Nose Inlets at Subcritical and Supercritical Mach Numbers