Search U.S. government technical reports digitized or harvested by TRAIL.
Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation
An analog study of a shock-position diffuser control on a supersonic turbojet engine
Some recent research on the handling qualities of airplanes
Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine
Flight and analytical study of roll requirements of a fighter airplane
The use of the horizontal tail for roll control
Factors affecting the maximum lift-drag ratio at high supersonic speeds
Spinning and related problems at high angles of attack for high-speed airplanes
Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion
A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05
Ditching Investigation of a 1/12-Scale Model of the Douglas F4D-1 Airplane, TED No. NACA DE 384
Low-speed static stability characteristics of a cambered-delta-wing model
Lift-curve slopes determined in flight on a flexible swept-wing jet bomber
Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7
Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers