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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


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