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- Effect of Thickness on the Lateral Force and Yawing Moment of a Sideslipping Delta Wing at Supersonic Speeds
- Thermodynamic Charts for Internal-Combustion-Engine Fluids
- Elastic Buckling of a Simply Supported Plate Under a Compressive Stress That Varies Linearly in the Direction of Loading
- Elastic Buckling of Outstanding Flanges Clamped at One Edge and Reinforced by Bulbs at Other Edge
- On Internal Damping of Rotating Beams
- NACA and Office of Naval Research Metallurgical Investigation of Two Large Forged Discs of S-590 Alloy
- Office of Naval Research and NACA Metallurgical Investigation of a Large Forged Disc of Inconel X Alloy
- Office of Naval Research and NACA Metallurgical Investigation of a Large Forged Disc of S-816 Alloy
- Experimental Investigation of Moving Pressure Disturbances and Shock Waves and Correlation with One-Dimensional Unsteady-Flow Theory
- Flight Investigation in Climb and at High Speed of a Two-Blade and a Three-Blade Propeller
- Matrix Methods for Calculating Cantilever-Beam Deflections
- A Comparison of Wing Loads Measured in Flight on a Fighter-Type Airplane by Strain-Gage and Pressure Distribution Methods
- Reinforced Circular Cutouts in Plane Sheets
- Quantitative Study of Variations in Concentration of Glycerol and Aerosol OT on Foaming Volume of Oil at Room Temperature
- Direct-Reading Design Charts for 24S-T Aluminum-Alloy Flat Compression Panels Having Longitudinal Formed Z-Section Stiffeners
- Summary of the Availability and Performance Problems of High Octane Number Fuels
- Preliminary Investigation of 3-Inch Slotted Transonic Wind-Tunnel Test Sections
- Spin-Tunnel Investigation of the Jettisoning of External Fuel Tanks in Spins
- Bibliography of Classified Aircraft-Fire Literature
- Study by NACA Wing-Flow Method of Transonic Drag Characteristics of a Blunt-Nose Body of Revolution and Comparison with Results for a Sharp-Nose Body
- Pressure Distributions on Thin Conical Body of Elliptic Cross Section at Mach Number 1.89
- Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges
- Investigation of Performance of Typical Inlet Stage of Multistage Axial-Flow Compressor
- Lateral-Control Investigation on a 37 Degree Sweptback Wing of Aspect Ratio 6 at a Reynolds Number of 6,800,000
- An Empirical Method for Estimating Trailing-Edge Loads at Transonic Speeds
- The Static-Pressure Error of Wing and Fuselage Airspeed Installations of the X-1 Airplanes in Transonic Flight
- Tests of the NACA 64-010 and 64A010 Airfoil Sections at High Subsonic Mach Numbers
- Investigation of Fretting by Microscopic Observation
- Effect of Reynolds Number in Turbulent-Flow Range on Flame Speeds of Bunsen Burner Flames
- Application of Radial-Equilibrium Condition to Axial-Flow Compressor and Turbine Design
- Line-Vortex Theory for Calculation of Supersonic Downwash
- Correlation of Physical Properties With Molecular Structure for Some Dicyclic Hydrocarbons Having High Thermal-Energy Release Per Unit Volume
- Equilibrium Operating Performance of Axial-Flow Turbojet Engines by Means of Idealized Analysis
- Plastic Buckling of a Rectangular Plate Under Edge Thrusts
- On Stability of Free Laminar Boundary Layer Between Parallel Streams
- Investigation of Separation of the Turbulent Boundary Layer
- Characteristics of Low-Aspect-Ratio Wings at Supercritical Mach Numbers
- Calculation of Counterrotating Propellers
- Behavior of the Laminar Boundary Layer for Periodically Oscillating Pressure Variation
- The Characteristics Method Applied to Stationary Two-Dimensional and Rotationally Symmetrical Gas Flows
- A Class of de Laval Nozzles
- Compression Shocks in Two-Dimensional Gas Flows
- The Effect of Air Jets Simulating Chines or Multiple Steps on the Hydrodynamic Characteristics of a Streamline Fuselage
- Summary of Information Relating to Gust Loads on Airplanes
- Stability Results Obtained With Douglas D-558-1 Airplane (BuAero No. 37971) in Flight Up to a Mach Number of 0.89
- Stability and Control Data Obtained from First Flight of X-4 Airplane
- Langley Free-Flight-Tunnel Investigation of the Automatic Lateral Stability Characteristics of a Model Equipped with a Gyro Stabilizing Unit that Provided either Flicker-Type or Hunting Control
- On Reflection of Shock Waves from Boundary Layers
- Investigation of Aerodynamic and Icing Characteristics of Recessed Fuel-Vent Configurations
- Investigation of Icing Characteristics of Typical Light Airplane Engine Induction Systems