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- NACA Mach Number Warning Device for Use in Flight
- Flight Studies of the Horizontal-Tail Loads Experienced by a Fighter Airplane in Abrupt Maneuvers
- Trends in Surface-Ignition Temperatures
- Relative Effects of Cylinder-Head and Inlet-Mixture Temperatures Upon Knock Limits of Fuels
- A Study of Piston and Ring Friction
- Résumé of NACA Stability and Control Tests of the Bell P-63 Series Airplane
- Profile Measurements During Cavitation
- Some Strength Tests of Stiffened Curved Sheets Loaded in Shear
- Spinning of Large Airplanes
- A Theoretical Investigation of Longitudinal Stability of Airplanes With Free Controls Including Effect of Friction in Control System
- Use of Water Injection to Decrease Gasoline Consumption in an Aircraft Engine Cruising at High Power
- Wind-Tunnel Investigation of an NACA 23021 Airfoil With a 0.32-Airfoil-Chord Double Slotted Flap
- Wind-Tunnel Investigation of Control-Surface Characteristics 16: Pressure Distribution Over an NACA 0009 Airfoil With 0.30-Airfoil-Chord Beveled-Trailing-Edge Flaps
- Wind-Tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface
- Wind-Tunnel Investigation of Shielded Horn Balances and Tabs on a 0.7-Scale Model of XF6F Vertical Tail Surface
- Vibration-Response Tests of a 1/5-Scale Model of the Grumman F6F Airplane in the Langley 16-Foot High-Speed Tunnel
- Effect of Compressibility on Pressure Distribution Over an Airfoil With a Slotted Frise Aileron
- The Effect of Oil Consumption and Piston Cooling on Knock-Limited Aircraft-Engine Performance
- Compressive Strength of Flat Panels with Z- and Hat-Section Stiffeners
- XC-35 Gust Research Project Analysis of Gust Measurements
- Tests of Hydraulically Expanded Rivets
- Nitrited-Steel Piston Rings for Engines of High Specific Power
- Wind-Tunnel Investigation of Control-Surface Characteristics 20: Plain and Balanced Flaps on an NACA 0009 Rectangular Semispan Tail Surface
- Tests of Thermal-Electric De-Icing Equipment for Propellers
- Tests of 10 Inch 24S-T Aluminum-Alloy Shear Panels With 1-1/2 Inch Holes 2: Panels Having Holes With Notched Edges
- Tests and Approximate Analysis of Bending Stresses Due to Torsion in a D-Section Box
- A Theoretical Investigation of the Rolling Oscillations of an Airplane With Ailerons Free
- Tests of Beams Having Webs With Large Circular Lightening Holes
- A Solution of the Direct and Inverse Potential Problems for Arbitrary Cascades of Airfoils
- An Interim Report on the Stability and Control of Tailless Airplanes
- An Experimental Investigation of the Flow of Air in a Flat Broadening Channel
- Experiments on Drag of Revolving Disks, Cylinders, and Streamline Rods at High Speeds
- Heat Transfer in a Turbulent Liquid or Gas Stream
- The Frictional Force with Respect to the Actual Contact Surface
- Gas Jets
- Bending and Shear Stresses Developed by the Instantaneous Arrest of the Root of a Cantilever Beam With a Mass at Its Tip
- Cowling and Cooling Tests of a Fleetwings Model 33 Airplane in Flight
- Effect of Lateral Shift of Center of Gravity on Rudder Deflection Required for Trim
- The Effect of Angle of Bend Between Plate Elements on the Local Instability of Formed Z-Sections
- Effect of Changes in Aileron Rigging on the Stick Forces of a High-Speed Fighter Airplane
- An Estimation of the Internal-Cooling Requirements of an Aircraft-Engine Cylinder When Using Oxygen Boost
- Estimates of the Vertical-Tail Loads of a Bell P-63A-1 Airplane (AAF No. 42-68889) in Accelerated Rolling Maneuvers Based on Flight Tests With Two Vertical-Tail Arrangements
- An Electronic Indicator for Angular Velocity and Acceleration
- Effect of Inlet-Air Temperature and Cylinder Displacement on Charge Temperature of Internal Combustion Engines
- Determination of Iron Contamination of Used Lubricating Oil for Use in Measuring Rates of Wear in Aircraft Engines
- Early Detection of Cracks Resulting From Fatigue Stressing
- The Effect of Compression Ratio on Knock Limits of High-Performance Fuels in a CFR Engine 1: Blends of Triptane and 28-R Fuel
- The Effects of a Highly Cambered Low-Drag Wing and of Auxiliary Flaps on the High-Speed Aerodynamic Characteristics of a Twin-Engine Pursuit Airplane Model
- Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-Dimensional Low-Turbulence Pressure Tunnel
- Analysis of Available Data on Control Surfaces Having Plain-Overhang and Frise Balances