Search U.S. government technical reports digitized or harvested by TRAIL.
Investigation of the Penetration of an Air Jet Directed Perpendicularly to an Air Stream
NACA Investigations of Icing-Protection Systems for Turbojet-Engine Installations
Experimental Investigation of Effect of Jet Exit Configuration on Thrust and Drag
Analytical Investigation of Icing Limit for Diamond-Shaped Airfoil in Transonic and Supersonic Flow
A Method for Rapid Determination of the Icing Limit of a Body in Terms of the Stream Conditions
Analogy Between Mass and Heat Transfer with Turbulent Flow
Investigation of Noise Field and Velocity Profiles of an Afterburning Engine
Investigation of noise field and velocity profiles of an afterburning engine
Investigation of Jet-Engine Noise Reduction by Screens Located Transversely Across the Jet
Investigation of Far Noise Field of Jets 1: Effect of Nozzle Shape