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- Free-jet altitude investigation of a 20-inch ram-jet combustor with a rich inner zone of combustion for improved low-temperature-ratio operation
- Effect of liner air-entry holes, fuel state, and combustor size on performance of an annular turbojet combustor at low pressures and high air-flow rates
- Effect of fuel injectors and liner design on performance of an annular turbojet combustor with vapor fuel
- Performance of an annular turbojet combustor having reduced pressure losses and using propane fuel
- An engineering method for the determination of aeroelastic effects upon the rolling effectiveness of ailerons on swept wings
- Small-scale transonic investigation of a 45 degree sweptback wing of aspect ratio 4 with combinations of nose-flap deflections and wing twist
- The effect of initial rate of subsonic diffusion on the stable subcritical mass-flow range of a conical shock diffuser
- An experimental study of five annular air inlet configurations at subsonic and transonic speeds
- Investigations toward simplification of missile control systems
- A study of the use of various high-lift devices on the horizontal tail of a canard airplane model as a means of increasing the allowable center-of-gravity travel
- Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings
- Impingement of Cloud Droplets on Aerodynamic Bodies as Affected by Compressibility of Air Flow Around the Body
- Procedure for Measuring Liquid-Water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method
- De-Icing and Runback Characteristics of Three Cyclic Electric, External De-Icing Boots Employing Chordwise Shedding
- Impingement of Water Droplets on a Cylinder in an Incompressible Flow Field and Evaluation of Rotating Multicylinder Method for Measurement of Droplet-Size Distribution, Volume-Median Droplet-Size, and Liquid-Water Content in Clouds
- Experimental Investigation of Radome Icing and Icing Protection
- Experimental Investigation of Laminar-Boundary-Layer Control on an Airfoil Section Equipped With Suction Slots Located at Discontinuities in the Surface Pressure Distribution
- Effect of Type of Porous Surface and Suction Velocity Distribution on the Characteristics of a 10.5 Percent-Thick Airfoil With Area Suction
- A Small Pirani Gage for Measurements of Nonsteady Low Pressures
- Theoretical Investigation of the Supersonic Lift and Drag of Thin, Sweptback Wings With Increased Sweep Near the Root
- A Low-Speed Experimental Study of the Directional Characteristics of a Sharp-Nosed Fuselage Through a Large Angle-of-Attack Range at Zero Angle of Sideslip
- The Drag of Finite-Length Cylinders Determined From Flight Tests at High Reynolds Numbers for a Mach Number Range From 0.5 to 1.3
- Estimation of Hydrodynamic Impact Loads and Pressure Distributions on Bodies Approximating Elliptical Cylinders With Special Reference to Water Landings of Helicopters
- Bearing Strengths of Some 75S-T6 and 14S-T6 Aluminum-Alloy Hand Forgings
- Calculation and Measurement of Normal Modes of Vibration of an Aluminum-Alloy Box Beam With and Without Large Discontinuities
- Application of Silver Chloride in Investigations of Elasto-Plastic States of Stress
- Column Strength of H-Sections and Square Tubes in Postbuckling Range of Component Plates
- An Investigation of the Experimental Aerodynamic Loading on a Model Helicopter Rotor Blade
- Effects of Parallel-Jet Mixing on Downstream Mach Number and Stagnation Pressure With Application to Engine Testing in Supersonic Tunnels
- Investigation of the Statistical Nature of the Fatigue of Metals
- The Creep of Single Crystals of Aluminum
- Subsonic Flow of Air Through a Single-Stage and a Seven-Stage Compressor
- Influence of Rotor-Engine Torsional Oscillation on Control of Gas-Turbine Engine Geared to Helicopter Rotor
- A Method for Calculating the Subsonic Steady-State Loading on an Airplane With a Wing of Arbitrary Plan Form and Stiffness
- A Study of the Stability of the Incompressible Laminar Boundary Layer on Infinite Wedges
- A Study of the Application of Power-Spectral Methods of Generalized Harmonic Analysis to Gust Loads on Airplanes
- The Structure of Turbulence in Fully Developed Pipe Flow
- A Digital Automatic Multiple Pressure Recorder
- Reflection of a Weak Shock Wave From a Boundary Layer Along a Flat Plate 1: Interaction of Weak Shock Waves With Laminar and Turbulent Boundary Layers Analyzed by Momentum-Integral Method
- Reflection of Weak Shock Wave From a Boundary Layer Along a Flat Plate 2: Interaction of Oblique Shock Wave With a Laminar Boundary Layer Analyzed by Differential-Equation Method
- The Galvanic Corrosion Theory for Adherence of Porcelain-Enamel Ground Coats to Steel
- Relation Between Roughness of Interface and Adherence of Porcelain Enamel to Steel
- Appraisal of Hazards to Human Survival in Airplane Crash Fires
- Supersonic Flow Past Oscillating Airfoils Including Nonlinear Thickness Effects
- Estimation of Forces and Moments Due to Rolling for Several Slender-Tail Configurations at Supersonic Speeds
- A Rapid Method for Use in Design of Turbines Within Specified Aerodynamic Limits
- Flow Properties of Strong Shock Waves in Xenon Gas as Determined for Thermal Equilibrium Conditions
- Counting Methods and Equipment for Mean-Value Measurements in Turbulence Research
- Deflection of Delta Wings Having a Carry-Through-Bay Chord Smaller than the Wing Root Chord
- The Effects of Camber on the Variation with Mach Number of the Aerodynamic Characteristics of a 10-Percent-Thick Modified NACA Four-Digit-Series Airfoil Section