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- A Simplified Method for Determining From Flight Data the Rate of Change of Yawing-Moment Coefficient With Sideslip
- Note on the Theorems of Bjerknes and Crocco
- Standard Nomenclature for Airspeeds With Tables and Charts for Use in Calculation of Airspeed
- The Synthesis and Purification of Aromatic Hydrocarbons 4: 1,2,3-Trimethylbenzene
- The Synthesis and Purification of Aromatic Hydrocarbons 1: Butylbenzene
- Standard Procedures for Rating and Testing Multistage Axial-Flow Compressors
- Methods for Determination and Computation of Flow Patterns of a Compressible Fluid
- Application of the Method of Characteristics to Supersonic Rotational Flow
- The Crystal Structure at Room Temperature of Eight Forged Heat-Resisting Alloys
- A General Method of Selecting Foam Inhibitors
- Experimental Determination of the Effects of Directional Stability and Rotary Damping in Yaw on Lateral Stability and Control Characteristics
- Quantitative Treatment of the Creep of Metals by Dislocation and Rate-Process Theories
- Pressure Distributions for Representative Airfoils and Related Profiles
- Summary and Analysis of Data on Damping in Yaw and Pitch for a Numbers of Airplane Models
- Consideration of Dynamic Loads on the Vertical Tail by the Theory of Flat Yawing Maneuvers
- Turbosupercharger-Rotor Temperatures in Flight
- Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow 1: Circulatory Flows Obeying the Simplified Density-Speed Relation
- A Condition on the Initial Shock
- The Lagrangian Multiplier Method of Finding Upper and Lower Limits to Critical Stresses of Clamped Plates
- Extension of the Chaplygin Proofs on the Existence of Compressible-Flow Solutions to the Supersonic Region
- A Discussion of the Application of the Prandtl-Glauert Method to Subsonic Compressible Flow Over a Slender Body of Revolution
- Stress Rupture of Heat Resisting Alloys as a Rate Process
- Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow 2: Subsonic Symmetric Adiabatic Flows
- On Supersonic and Partially Supersonic Flows
- Wind-Tunnel Investigation of the Effect of Canopies on Directional Stability Characteristics of a Single Engine Airplane Model
- Lifting-Surface-Theory Results for Thin Elliptic Wings of Aspect Ratio 3 with Chordwise Loadings Corresponding to 0.5-Chord Plain Flap and to Parabolic-Arc Camber
- Column Strength of Aluminum Alloy 14S-T Extruded Shapes and Rod
- Stress-Strain and Elongation Graphs for Aluminum Alloy R301 Sheet
- Effects of Axial-Plane Curvature and Passage-Area Variation on Flow Capacity of Radial-Discharge Impeller with Conventional Inlet Buckets
- Effects of Tip Dihedral on Lateral Stability and Control Characteristics as Determined by Tests of a Dynamic Wind Model in the Langley Free-Flight Tunnel
- Performance Parameters for Jet-Propulsion Engines
- A Relaxation Procedure for the Stress Analysis of a Continuous Beam-Column Elastically Restrained Against Deflection and Rotation at the Supports
- Impact Strength and Flexural Properties of Laminated Plastics at High and Low Temperatures
- Flight and Test-Stand Investigation of High-Performance Fuels in Pratt & Whitney R-1830-94 Engines 4: Comparison of Cooling Characteristics of Flight and Test-Stand Engines
- Theory and Application of Hot-Wire Instruments in the Investigation of Turbulent Boundary Layers
- Preliminary Investigation of a New Type of Supersonic Inlet
- Effect of Compressibility at High Subsonic Velocities on the Lifting Force Acting on an Elliptic Cylinder
- Flight Investigation at High Speeds of the Drag of Three Airfoils and a Circular Cylinder Representing Full-Scale Propeller Shanks
- Application of the Analogy Between Water Flow With a Free Surface and Two-Dimensional Compressible Gas Flow
- Investigations of Effects of Surface Temperature and Single Roughness Elements on Boundary-Layer Transition
- Investigations on Laminar Boundary-Layer Stability and Transition on Curved Boundaries
- Effect of Rotor-Tip Speed on Helicopter Hovering Performance and Maximum Forward Speed
- Effects of Specific Types of Surface Roughness on Boundary-Layer Transition
- Quantitative Treatment of the Creep of Metals by Dislocation and Rate-Process Theories
- Air-Flow and Performance Characteristics of Engine-Stage Supercharger of a Double-Row Radial Aircraft Engine 2: Effect of Design Variables
- Consideration of Dynamic Loads on the Vertical Tail by the Theory of Flat Yawing Maneuvers
- Occurrence of Iron Oxides on Cast-Iron Engine Surfaces After Operation
- JRM-1 Landing Impact Characteristics From Model Tests
- The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight
- A Thermodynamic Study of the Turbojet Engine