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- 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
- Preliminary Investigation of the Transonic Characteristics of an NACA Submerged Inlet
- Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured on the Wing of the Bell X-1 Airplane in Level Flight at Mach Numbers From 0.79 to 1.00 and in a Pull-Up at a Mach Number of 0.96
- A Transonic Wing Investigation in the Langley 8-Foot High-Speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2 : Wing-Fuselage Configuration Having a Wing of 35 Degrees Sweepback, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section
- The Time Lag Between Flap Deflection and Force Development at a Mach Number of 4
- Transonic Drag Characteristics of a Wing Body Combination Using a Thin Tapered Wing of 45 Degrees Sweepback
- Propeller Section Aerodynamic Characteristics as Determined by Measuring the Section Surface Pressures on an NACA 10-(3)(08)-03 Propeller Under Operating Conditions
- Results Obtained During Flights 1 to 6 of the Northrop X-4 Airplane (A.F. No. 46-677)
- Summary of Normal Accelerations, Gust Velocities, and Operating Practices, From April to August 1949 of a Twin-Engine Airplane in Commercial Transport Operations
- Rolling Effectiveness of a Thin Tapered Wing Having Partial-Span Ailerons as Determined by Rocket-Powered Test Vehicles
- The Rolling Effectiveness of Wing-Tip Ailerons as Determined by Rocket-Powered Test Vehicles and Linear Supersonic Theory
- Pressure Distributions on the Blade Sections of the NACA 10-(3)(066)-033 Propeller Under Operating Conditions
- Pressure Distributions on the Blade Sections of the NACA 10-(5)(066)-03 Propeller Under Operating Conditions
- Pressure Distributions on the Blade Sections of the NACA 10-(3)(049)-033 Propeller Under Operating Conditions
- Pressure Distributions on the Blade Sections of the NACA 10-(0)(066)-03 Propeller Under Operating Conditions
- Pressure Distributions on the Blade Sections of the NACA 10-(3)(090)-03 Propeller Under Operating Conditions