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- The Shock-Absorbed System of the Airplane Landing Gear
- Standards for Discharge Measurement With Standardized Nozzles and Orifices
- Tests of Lead-Bronze Bearings in the DVL Bearing-Testing Machine
- Testing of High-Octane Fuels in the Single-Cylinder Airplane Engine
- Italian High-Speed Airplane Engines
- Limits of Single-Stage Compression in Centrifugal Superchargers for Aircraft
- Experimental Investigation to Determine the Relative Magnitude of Vertical and Horizontal Gusts in the Atmosphere
- Experimental Results With Airfoils Tested in the High-Speed Tunnel at Guidonia
- General Relationships Between the Various Systems of Reference Axes Employed in Flight Mechanics
- The Cause of Welding Cracks in Aircraft Steels
- Theoretical and Experimental Investigations of the Drag of Installed Aircraft Radiators
- The Strength of Shell and Tubular Spar Wings
- Some Data on the Static Longitudinal Stability and Control of Airplanes: Design of Control Surfaces
- Knocking in an Internal-Combustion Engine
- Chordwise Load Distribution of a Simple Rectangular Wing
- DFS Dive-Control Brakes for Gliders and Airplanes and Analytical Study of the Drag of the DFS Dive-Control Brake
- Rectangular Shell Plating Under Uniformly Distributed Hydrostatic Pressure
- Materials for Slack Diaphragms
- Wind Tunnel Tests of a Submerged-Engine Fuselage Design
- Variation in Velocity Profile with Change in Surface Roughness of Boundary
- Wind-Tunnel Investigation of Spoiler, Deflector, and Slot Lateral-Control Devices on Wings With Full-Span Split and Slotted Flaps
- Investigations on the Incompletely Developed Plane Diagonal-Tension Field
- Tensile Elastic Properties of Typical Stainless Steels and Nonferrous Metals as Affected by Plastic Deformation and by Heat Treatment
- Stress Distribution in and Equivalent Width of Flanges of Wide, Thin-Wall Steel Beams
- Analysis and Prediction of Longitudinal Stability of Airplanes
- A Method of Measuring Piston Temperatures
- The Effects of Piston-Head Shape, Cylinder-Head Shape, and Exhaust Restriction, on the Performance of a Piston-Ported Two-Stroke Cylinder
- Drag Determinations of the Forward Component of a Tricycle Landing Gear
- Internal-Flow Systems for Aircraft
- Correlation of knocking characteristics of fuels in an engine having a hemispherical combustion chamber
- Damping formulas and experimental values of damping in flutter models
- Transient effects of the wing wake on the horizontal tail
- Tests of a gust-alleviating flap in the gust tunnel
- Wind tunnel tests of an NACA 23021 airfoil equipped with a slotted extensible and a plain extensible flap
- A Flight Investigation of Exhaust-Heat De-Icing
- Flight investigation of control-stick vibration of the YG-1B autogiro
- The effects of engine speed and mixture temperature on the knocking characteristics of several fuels
- An Investigation of the Prevention of Ice on the Airplane Windshield
- Pressure-distribution investigation on an NACA 0009 airfoil with a 30-percent-chord plain flap and three tabs
- A study of unsymmetrical-loading conditions
- A study of the air movement in two aircraft-engine cylinders
- Wind-tunnel investigation of an NACA 23030 airfoil with various arrangements of slotted flaps
- Notes on the stalling of vertical tail surfaces and on fin design
- Pressure-distribution investigation of an NACA 0009 airfoil with an 80-percent-chord plain flap and three tabs
- Wind tunnel investigation of fuselage stability in yaw with various arrangements of fins
- Wind-tunnel investigation of two airfoils with 25-percent-chord Gwinn and plain flaps
- On the Theory of Unsteady Planing and the Motion of a Wing With Vortex Separation
- Preliminary Tests in the NACA Tank to Investigate the Fundamental Characteristics of Hydrofoils
- Requirements for Unit Fuel-Injection Systems
- Wind-Tunnel Investigation of Rectangular Air-Duct Entrances in the Leading Edge of an NACA 23018 Wing, Special Report