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- Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Transonic Speeds
- Turbojet Propulsion-System Research and the Resulting Effects on Airplane Performance
- Emergency Spin-Recovery Device for the 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel
- Aerodynamic Design of Axial-Flow Compressors. VII - Blade-Element Flow in Annular Cascades
- Transonic Zero-Lift Drag Tests of Four Equivalent-Body-of-Revolution Models Representing Variations of the Convair F-102 Airplane
- Free-Spinning and Recovery Characteristics of a 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel
- Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8
- Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination
- A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body
- Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions
- 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
- Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron
- Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase against maneuvering and nonmaneuvering targets
- Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6
- NACA Conference on engine stall and surge
- Preliminary analysis of performance of turbojet engines used as pumps for boundary-layer control
- Variation of Local Liquid-Water Concentration About an Ellipsoid of Fineness Ratio 10 Moving in a Droplet Field
- Full-scale, free-jet investigation of methods of improving outlet flow distribution in a side-inlet supersonic diffuser
- Impingement of Water Droplets on a Sphere
- Impingement of Water Droplets on NACA 65A004 Airfoil at 0 Deg Angle of Attack
- Preliminary Data on Rain Deflection from Aircraft Windshields by Means of High-Velocity Jet-Air Blast
- An Investigation of the Effects of Nose and Lip Shapes for an Underslung Scoop Inlet at Mach Numbers from 0 to 1.9
- Performance Characteristics of Several Divergent-Shroud Aircraft Ejectors
- Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
- Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method
- Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8
- Exploratory investigation of an airfoil with area suction applied to a porous, round trailing edge fitted with a lift-control vane
- Flight testing by radio remote control-flight evaluation of a beep-control system
- Free-spinning-tunnel investigation of gyroscopic effects of jet-engine rotating parts (or of rotating propellers)
- Chain breaking and branching in the active-particle diffusion concept of quenching
- Chemical Action of Halogenated Agents in Fire Extinguishing
- Intergranular corrosion of high-purity aluminum in hydrochloric acid II : grain-boundary segregation of impurity atoms
- Intergranular corrosion of high-purity aluminum in hydrochloric acid I : effects of heat treatment, iron content, and acid composition
- Interaction of a free flame front with a turbulence field
- Ingestion of foreign objects into turbine engines by vortices
- Investigation of temperature limitation of various lubricants for high-temperature 20-millimeter-bore ball bearings
- Investigation of the vibrations of a hollow thin-walled rectangular beam
- An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2
- Method for rapid graphical evaluation of cooled or uncooled turbojet and turboprop engine or component performance (effects of variable specific heat included)
- Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings
- 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