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- Investigation of downwash and wake characteristics at a Mach number of 1.53 3: swept wings
- Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds: wing and fuselage pressure distribution
- Turbojet combustion efficiency at high altitudes
- Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds
- Comparison of outside-surface heat-transfer coefficients for cascades of turbine blades
- Spontaneous ignition temperatures of pure hydrocarbons and commercial fluids
- Aeronautical study of a wing-fuselage combination employing a wing swept back 63 degrees: Characteristics at supersonic speeds of a model with the wing twisted and cambered for uniform load
- Investigation of the downwash and wake behind a triangular wing of aspect ratio 4 at subsonic and supersonic Mach numbers
- Investigation of effects of inlet-air velocity distortion on performance of turbojet engine
- Wind-tunnel investigation of a 1/6-scale model of the Bumblebee XPM missile at high subsonic speeds
- Wind-tunnel investigation at Mach numbers of 2.0 and 2.9 of several configurations of a supersonic ram-jet test vehicle
- Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane
- Investigation of effect of span and spanwise location of plain and stepped spoiler ailerons on lateral control characteristics of a wing with leading edge swept back 51.3 degrees
- Factors in selecting fuels for gas-turbine powered aircraft
- Extension of boundary-layer heat-transfer theory to cooled turbine blades
- Experimental investigation of thrust augmentation of 4000-pound-thrust axial-flow-type turbojet engine by interstage injection of water-alcohol mixtures in compressor
- Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by bleedoff
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: effect of Reynolds number at supersonic Mach numbers on the longitudinal characteristics of a wing twisted and cambered for uniform load
- Altitude performance characteristics of tail-pipe burner with variable-area exhaust nozzle
- Altitude-wind-tunnel investigation of tail-pipe burner with converging conical burner section on J35-A-5 turbojet engine
- Effects of boundary-layer control on the longitudinal characteristics of a 45 degrees swept-forward wing-fuselage combination
- Altitude-wind-tunnel investigation of turbine performance in J47 turbojet engine
- A preliminary flight investigation of the effects of vortex generators on separation due to shock
- Longitudinal characteristics of two 47.7 degree sweptback wings with aspect ratios of 5.1 and 6.0 at Reynolds numbers up to 10 x 10(exp 6)
- Effects of leading-edge devices and trailing-edge flaps on longitudinal characteristics of two 47.7 degree sweptback wings of aspect ratios 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)
- Supplementary analysis of the dynamic lateral stability characteristics of the Bell X-2 airplane as affected by variations in mass and aerodynamic parameters
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of sideslip on aerodynamic characteristics at a Mach number of 1.4 with the wing twisted and cambered
- Free-flight investigation at transonic and supersonic speeds of the rolling effectiveness of a partial-span aileron on an inversely tapered sweptback wing
- On the Formation of Shock Waves in Subsonic Flows With Local Supersonic Velocities
- Large-Scale Flight Measurements of Zero-Lift Drag at Mach Numbers from 0.90 to 1.95 of 1/14-Scale Model of the Northrop MX-775B Pilotless Aircraft with Small Body
- Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine
- Further experiments on the flow and heat transfer in a heated turbulent air jet
- Fundamental effects of aging on creep properties of solution-treated low-carbon n-155 alloy
- Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design
- Horizontal tail loads in maneuvering flight
- Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data
- Measurements of average heat-transfer and friction coefficients for subsonic flow of air in smooth tubes at high surface and fluid temperatures
- General algebraic method applied to control analysis of complex engine types
- Determination of plate compressive strengths at elevated temperatures
- The aerodynamic forces on slender plane- and cruciform-wing and body combinations
- Analysis of spanwise temperature distribution in three types of air-cooled turbine blade
- Blockage corrections for three-dimensional-flow closed-throat wind tunnels, with consideration of the effect of compressibility
- Effect on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system
- The effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x 10sub6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections
- Performance of J33-A-27 Turbojet-Engine Compressor, III, Over-All Performance Characteristics of Modified Compressor with Water Injection at Design Equivalent Speed of 11,800 RPM
- Effect of an Autopilot Sensitive to Yawing Velocity on the Lateral Stability of the Douglas D-558-II Airplane
- Results of the Flight Test of a Dummy of the MX-656 Rocket-Propelled Models
- Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip
- Preliminary Performance Data on General Electric Integrated Electronic Control Operating on J47 RX1-3 Turbojet Engine in NACA Altitude Wind Tunnel
- Investigation of Performance of Axial-Flow Compressor of XT-46 Turbine-Propeller Engine 2 - Performance of Revised Compressor at Design Equivalent Speed