Search U.S. government technical reports digitized or harvested by TRAIL.
Turbojet Propulsion-System Research and the Resulting Effects on Airplane Performance
Aerodynamic Design of Axial-Flow Compressors. VII - Blade-Element Flow in Annular Cascades
Loads on thin wings at transonic speeds
A study of means for rationalizing airplane design loads
Landing conditions for large airplanes in routine operations
Some factors affecting the variation of pitching moment with sideslip of aircraft configurations
NACA Conference on engine stall and surge
Preliminary analysis of performance of turbojet engines used as pumps for boundary-layer control
Impingement of Water Droplets on a Sphere
Impingement of Water Droplets on NACA 65A004 Airfoil at 0 Deg Angle of Attack
Performance Characteristics of Several Divergent-Shroud Aircraft Ejectors
Flight testing by radio remote control-flight evaluation of a beep-control system
Chain breaking and branching in the active-particle diffusion concept of quenching
Chemical Action of Halogenated Agents in Fire Extinguishing
Interaction of a free flame front with a turbulence field
Ingestion of foreign objects into turbine engines by vortices
Investigation of the vibrations of a hollow thin-walled rectangular beam
Noise survey of a 10-foot four-blade turbine-driven propeller under static conditions
NACA model investigations of seaplanes in waves
An NACA vane-type angle-of-attack indicator for use at subsonic and supersonic speeds
Preliminary investigation of a stick shaker as a lift-margin indicator
Laminar separation over a transpiration-cooled surface in compressible flow
Longitudinal turbulent spectrum survey of boundary layers in adverse pressure gradients
A low-density wind-tunnel study of shock-wave structure and relaxation phenomena in gases