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- Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41
- Some Features of Artificially Thickened Fully Developed Turbulent Boundary Layers with Zero Pressure Gradient
- Small Bending and Stretching of Sandwich-Type Shells
- Supersonic Flow Around Circular Cones at Angles of Attack
- A General Integral Form of the Boundary-Layer Equation for Incompressible Flow With an Application to the Calculation of the Separation Point of Turbulent Boundary Layers
- The External-Shock Drag of Supersonic Inlets Having Subsonic Entrance Flow
- Preliminary Investigation of Reflections of Oblique Waves from a Porous Wall
- Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine: 1: Rotor Blades With 10 Tubes in Cooling-Air Passages
- Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds: Tail Attached to a Segment of the Foreshortened Body
- Wind-Tunnel Investigation of a 1/6-Scale Model of the Bumblebee XPM Missile at High Subsonic Speeds
- Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 2: Rotor Blades With 15 Fins in Cooling-Air Passages
- Effect of Nose Shape and Wing Thickness Ratio on the Drag at Zero Lift of a Missile Having Triangular Wings and Tails
- Investigation of Power Requirements for Ice Prevention and Cyclical De-Icing of Inlet Guide Vanes with Internal Electric Heaters
- Model Ditching Investigations of Three Airplanes Equipped With Hydro-Skis
- Photomicrographic Investigation of Spontaneous Freezing Temperatures of Supercooled Water Droplets
- The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment
- Investigation of Aerodynamic and Icing Characteristics of Water-Inertia-Separation Inlets for Turbojet Engines
- Improvements in Heat Transfer for Anti-Icing of Gas-Heated Airfoils with Internal Fins and Partitions
- Blockage Corrections for Three-Dimensional-Flow Closed-Throat Wind Tunnels, with Consideration of the Effect of Compressibility
- Flight investigation of the effect of transient wing response on measured accelerations of a modern transport airplane in rough air
- Prandtl-Meyer Flow for a Diatomic Gas of Variable Specific Heat
- Tables for Determining Reduction of Energy and Intensity of X-Rays and Gamma-Rays at Various Scattering Angles in Small Thickness of Matter
- A Review of Information on the Mechanical Properties of Aluminum Alloys at Low Temperatures
- Water Landing Investigation of a Model Having a Heavy Beam Loading and a 30 Degree Angle of Dead Rise
- Investigation of a Two-Step Nozzle in the Langley 11-Inch Hypersonic Tunnel
- A Theoretical Investigation of the Effect on the Lateral Oscillations of an Airplane of an Automatic Control Sensitive to Yawing Accelerations
- Effect of Humidity on Performance of Turbojet Engines
- Effect of Heat-Capacity Lag on the Flow Through Oblique Shock Waves
- Bonding Investigation of Titanium Carbide With Various Elements
- Analytical Method for Determining Transmission and Absorption of Time-Dependent Radiation Through Thick Absorbers 3: Absorber With Radioactive Daughter Products
- An Investigation of the Effect of Tetraethyl Lead and Ethyl Nitrite on the Autoignition Characteristics of Isooctane and Triptane
- Knock-Limited Performance of Fuel Blends Containing Ethers
- Method for Determining Pressure Drop of Air Flowing Through Constant-Area Passages for Arbitrary Heat-Input Distributions
- Linearized Supersonic Theory of Conical Wings
- Effect of Initial Mixture Temperature on Flame Speeds and Blow-Off Limits of Propane - Air Flames
- Hovering and Low-Speed Performance and Control Characteristics of an Aerodynamic-Servocontrolled Helicopter Rotor System as Determined on the Langley Helicopter Tower
- Shear Stress Distribution Along Glue Line Between Skin and Cap-Strip of an Aircraft Wing
- Free Oscillations of an Atmosphere in Which Temperature Increases Linearly With Height
- Strength Properties of Rayon-Mat Honeycomb Core Materials
- Analysis of V-g data obtained from several naval airplanes
- Planing Characteristics of Six Surfaces Representative of Hydro-Ski Forms
- Performance of Three High-Recovery-Factor Thermocouple Probes for Room-Temperature Operation
- A Preliminary Experimental and Analytical Evaluation of Diborane as a Ram-Jet Fuel
- Preliminary Investigation of a Submerged Air Scoop Utilizing Boundary-Layer Suction to Obtain Increased Pressure Recovery
- Exploratory Investigation of Leading-Edge Chord-Extensions to Improve the Longitudinal Stability Characteristics of Two 52 Degree Sweptback Wings
- Flight Investigation at Mach Numbers From 0.8 to 1.4 to Determine the Zero-Lift Drag of Wings With 'M' and 'W' Plan Forms
- Experimental Investigation of Various Wing-Mounted External Stores on a Wing-Fuselage Combination Having a Sweptback Wing of Inverse Taper Ratio
- Experimental Investigation of Various External-Store Configurations on a Model of a Tailless Airplane With a Sweptback Wing
- An Experimental Investigation at Large Scale of an NACA Submerged Intake and Deflector Installation on the Rearward Portion of a Fuselage
- Some Effects of Chordwise Fences on the Aerodynamic Characteristics of Four Moderately Sweptback Wings in the Low-Lift Range at Transonic Mach Numbers and at Mach Number 1.9