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- Test of NACA 66,2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
- Contribution to the ideal efficiency of screw propellers
- Normal-pressure tests of circular plates with clamped edges
- Beam and torsion tests of aluminum-alloy 615-T tubing
- Bending tests of a monocoque box
- Bending with large deflection of a clamped rectangular plate with length-width ratio of 1.5 under normal pressure
- Ground effect on downwash angles and wake location
- Stability of elastically supported columns
- The effect of exhaust-stack shape on the design and performance of the individual cylinder exhaust-gas jet-propulsion system
- A method for calculating heat transfer in the laminar flow region of bodies
- A method for determining the rate of heat transfer from a wing or streamline body
- The Tracer Gas Method of Determining the Charging Efficiency of Two-Stroke-Cycle Diesel Engines
- The Limiting Useful Deflections of Corrugated Metal Diaphragms
- Investigation of the Forces Acting on Gliders in Automobile-, Pulley-, Winch-, and Airplane Towed Flight
- Curing of Resin-Wood Combinations by High-Frequency Heating
- Improvement of Fatigue Life of an Aluminum Alloy by Overstressing
- Stress Analysis of Monocoque Fuselage Bulkheads by the Photoelastic Method
- A Rosette Strain Computer
- A Preliminary Investigation of the Electrical Structure of Thunderstorms
- A Method for Determining the Camber and Twist of a Surface to Support a Given Distribution of Lift
- Tidewater and Weather-Exposure Tests on Metals Used in Aircraft - 2
- On the Distribution of Stress in a Thin Plate Elastically Supported Along Two Edges at Loads Beyond the Stability Limit
- Tensile and Pack Compressive Tests of Some Sheets of Aluminum Alloy, 1025 Carbon Steel, and Chromium-Nickel Steel
- Tests of Propeller-Speed Cooling Blowers
- Investigation of Lubricants Under Boundary Friction
- Propeller Selection From Aerodynamic Considerations
- On the Symmetrical Potential Flow of Compressible Fluid Past a Circular Cylinder in the Tunnel in the Subcritical Zone
- Progress Summary Number 1: Mechanical Properties of Flush-Riveted Joints Submitted by Five Airplane Manufacturers
- XC-35 Gust Research Project Operation in Cumulus Congestus Cloud on July 31, 1941 Maximum Gust Intensities
- Statics of Circular-Ring Stiffeners for Monocoque Fuselages
- Stalling Characteristics of the Supermarine Spitfire VA Airplane
- Tests of a Stressed-Carrying Door in Shear
- Tests of a Stress-Carrying Door in Compression
- A Method of Shear-Lag Analysis of Box Beams for Axial Stresses, Shear Stresses, and Shear Center
- Notes on the Effects of Trailing-Edge Shapes of Low-Drag Airfoils on Profile Drag and the Trim and Balance of Control Surfaces
- Effect of Aromatics and Spark Advance on Thermal Efficiency
- A Description of the Ju 88 Airplane Anti-Icing Equipment
- A Flight Investigation of the Stability of a Towed Body
- Flight Investigation of the Performance and Cooling Characteristics of an NACA C Cowling on the XP-42 Airplane
- The Design of Propeller Blade Roots
- High-Speed Wind-Tunnel Tests of a 1/6-Scale Model of a Twin-Engine Pursuit Airplane
- Control-Motion Studies of the PBM-3 Flying Boat in Abrupt Pull-Ups
- The Development of Satisfactory Flying Qualities on the Douglas Dive Bomber, Model SBD-1 Through Flight Testing Successive Modifications in Control-Surface Area, Hinge-Line Location, and Aerodynamic-Balance Nose Shape
- Effect of Ground on Characteristics of Model of a Low-Wing Airplane With Full-Span Slotted Flap With and Without Power
- Elevator Stick Forces in Spins as Computed From Wind-Tunnel Measurements
- Prediction of Downwash and Dynamic Pressure at the Tail From Free-Flight Measurements
- The Strength and Stiffness of Shear Webs With and Without Lightening Holes
- Strength Tests on Hulls and Floats
- Construction of Finned Aluminum Muffs for Aircraft Engine Cylinder Barrels
- Theoretical Distribution of Load Over a Swept-Back Wing