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- The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-Flight Tunnel
- Effect of a Trailing-Edge Extension on the Characteristics of a Propeller Section
- Simple Curves for Determining the Effects of Compressibility on Pressure Drop Through Radiators
- High-Altitude Cooling 3: Radiators
- Effect of Fuel Volatility on Performance of a Wright R-2600-8 Engine as Influenced by Mixture Distribution
- Wind-Tunnel Investigation of Carburetor Air Scoops for the XTB2D-1 Airplane with Emphasis on Means for Bypassing the Boundary Layer
- Wind-Tunnel Investigation of Ailerons on a Low-Drag Airfoil 3: The Effect of Tabs
- The Effect of Engine Conditions on the Lead Susceptibility of Paraffinic Fuels
- Experimental Study of the Coating Found on Scuffed Cast-Iron Piston Rings During Operation in Nitrided-Steel Cylinders
- Wind-Tunnel Investigation of a Beveled Aileron Shape Designed to Increase the Useful Deflection Range
- Tests of NACA 65(216)-420 and 66(218)-420 Airfoils at High Speeds
- Cylinder-Head Cooling by Means of a Shield in the Exhaust Passage
- Air-Consumption Parameters for Automatic Mixture Control of Aircraft Engines
- Determination of the Stresses Produced by the Landing Impact in the Bulkheads of a Seaplane Bottom
- Comparative Results of Tests on Several Different Types of Nozzles
- Compressibility Effects on Heat Transfer and Pressure Drop in Smooth Cylindrical Tubes
- Determination of the Actual Contact Surface of a Brush Contact
- DVL Angular Velocity Recorder
- Simply Supported Long Rectangular Plate Under Combined Axial Load and Normal Pressure
- On the General Theory of Thin Airfoils for Nonuniform Motion
- The "Limiting Line" in Mixed Subsonic and Supersonic Flow of Compressible Fluids
- Dynamics of the Inlet System of a Four-Stroke Engine
- The Conformal Transformation of an Airfoil Into a Straight Line and Its Application to the Inverse Problem of Airfoil Theory
- The Influence of the Aerodynamic Span Effect on the Magnitude of the Torsional-Divergence Velocity and on the Shape of the Corresponding Deflection Mode
- Fairing Compositions for Aircraft Surfaces
- The Effect of Increased Cooling Surface on Performance of Aircraft-Engine Cylinders as Shown by Tests of the NACA Cylinder
- Wind-Tunnel Tests of the 1/8-Scale Powered Model of the Curtiss XBTC-2 Airplane 1: Preliminary Investigation of Longitudinal Stability
- Ovalization of Tubes Under Bending and Compression
- Power-Off Tests of the Northrop N9M-2 Tailless Airplane in the 40- by 80-Foot Wind Tunnel
- High-Altitude Cooling 3: Radiators
- Flight Tests of the High-Speed Performance of a P-51B Airplane (AAF No. 43-12105)
- Applicability of Similarity Principles to Structural Models
- A Least-Squares Procedure for the Solution of the Lifting-Line Integral Equation
- Piloting of flying boats with special reference to porpoising and skipping
- Notes on Unusual V-G Records From Transport Airplanes
- The Effect of Increased Cooling Surface on Performance of Aircraft-Engine Cylinders as Shown by Tests of the NACA Cylinder
- A Comparison of the Effects of Four-Blade Dual- and Single-Rotation Propellers on the Stability and Control Characteristics of a High-Powered Single-Engine Airplane
- Performance of Blowdown Turbine Driven by Exhaust Gas of Nine-Cylinder Radial Engine
- Preliminary Investigation of the Relation of the Compressive Strength of Sheet-Stiffener Panels to the Diameter of Rivet Used for Attaching Stiffeners to Sheet
- Preliminary Tank Experiments With a Hydrofoil on a Planing-Tail Seaplane Hull
- Flight and Test-Stand Investigation of High-Performance Fuels in Double-Row Radial Air-Cooled Engines 1: Determination of Cooling Characteristics of Flight Engine
- Extended Tables of Stiffness and Carry-Over Factor for Structural Members Under Axial Load
- F-3 and F-4 Engine Tests of Several High-Antiknock Components of Aviation Fuel
- Flight and Test-Stand Investigation of High-Performance Fuels in Double-Row Radial Air-Cooled Engines 2: Flight Knock Data and Comparison of Fuel Knock Limits With Engine Cooling Limits in Flight
- Flight Investigation at High Mach Numbers of Several Methods of Measuring Static Pressure on an Airplane Wing
- Tank Tests on the Resistance and Porpoising Characteristics of Three Flying-Boat Hull Models Equipped With Planing Flaps
- Some Effects of Propeller Operation on the Distribution of the Load on the Vertical Tail Surface of a Typical Pursuit Airplane
- Stability of a Body Stabilized by Fins and Suspended From an Airplane
- Shear-Lag Tests of Two Box Beams With Corrugated Covers Loaded to Failure
- Significance of Alkylate-Replacement Values of Aviation Fuel Components