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• Cooling and Performance Tests of a Continental A-75 Engine
• Stresses and Deflections in Thin Shells and Curved Plates Due to Concentrated and Variously Distributed Loading
• The Tensile Elastic Properties at Low Temperatures of 18:8 Cr-Ni Steel as Affected by Heat Treatment and Slight Plastic Deformation
• Variation of Properties Throughout Cross Section of Two Extruded Shapes
• Tests of Bell XP-63 Low-Drag Wing Model With Split Flap
• New Method of Calculating the Power at Altitude of Aircraft Engines Equipped With Superchargers on the Basis of Tests Made Under Sea-Level Conditions
• The Oscillating Wing With Aerodynamically Balanced Elevator
• On the Use of Residue Theory for Treating the Subsonic Flow of a Compressible Fluid
• Researches on Direct Injection in Internal-Combustion Engines
• Determination of the Bending and Buckling Effect in the Stress Analysis of Shell Structures Accessible From One Side Only
• Static Characteristics of Hamilton Standard Propellers Having Clark Y and NACA 16 Series Blade Sections
• Tests of a 0.1475c Aileron With a Tab on Low-Drag Section for Curtiss XP-60 Airplane in the Low-Turbulence Tunnel
• Static Characteristics of Curtiss Propellers Having Different Blade Sections
• Experimental Investigations on Freely Exposed Ducted Radiators
• Dynamic Similitude in Internal-Combustion Engines
• A Flight Investigation of Internally Balanced Sealed Ailerons
• Comparison of Automatic Control Systems
• The Creep of Laminated Synthetic Resin Plastics
• The Design of Jet Pumps
• The Elliptic Wing Based on the Potential Theory
• The Reaction Jet as a Means of Propulsion at High Speeds
• Stress Analysis of Circular Frames
• Use of Charts for Flow Discharge Calculations
• Wind-Tunnel Investigation of Control-Surface Characteristics 3: A Small Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
• Wind-Tunnel Investigation of Control-Surface Characteristics 4: A Medium Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
• Inertia of Dynamic Pressure Arrays
• Square Plate With Clamped Edges Under Normal Pressure Producing Large Deflections
• Stagnation Temperature Recording
• Contribution to the Aerodynamics of Rotating-Wing Aircraft: Part 2
• Observations of the Effect of Wing Appendages and Flaps on the Spread of Separation of Flow Over the Wing
• Requirements for Satisfactory Flying Qualities of Airplanes
• Wind-Tunnel Investigation of a Plain and a Slot-Lip Aileron on a Wing With a Full-Span Flap Consisting of an Inboard Fowler and an Outboard Slotted Flap
• Effect of Threaded and Serrated Holes on the Limited Time and Fatigue Strength of Flat Light-Alloy Strips
• On the Calculation of Flow Past an Infinite Screen of Thin Airfoils
• Factors Influencing the Fatigue Strength of Materials
• The Efficiency of Combustion Turbines With Constant-Pressure Combustion
• The Mechanical Properties of Wood of Different Moisture Content Within -200 Degrees to +200 Degrees C Temperature Range
• Effect of Aging on Mechanical Properties of Aluminum-Alloy Rivets
• Wind-Tunnel Investigation of an NACA 23021 Airfoil With Two Sizes of Balanced Split Flaps
• Boundary Layer Removal by Suction
• Wind-Tunnel Development of a Plug-Type Spoiler-Slot Aileron for a Wing With a Full-Span Slotted Flap and a Discussion of Its Application
• Tank Tests of a 1/5 Full-Size Dynamically Similar Model of the Army OA-9 Amphibian With Motor-Driven Propellers: NACA Model 117
• Requirements for Satisfactory Flying Qualities of Airplanes
• Characteristics of Naca 4400R Series Rectangular and Tapered Airfoils, Including the Effect of Split Flaps
• Development of Cowling for Long-Nose Air-Cooled Engine in the NACA Full-Scale Wind Tunnel
• Lateral Control Required for Satisfactory Flying Qualities Based on Flight Tests of Numerous Airplanes
• Tests of the NACA 0025 and 0035 Airfoils in the Full-Scale Wind Tunnel
• The Compressive Yield Strength of Extruded Shapes of 24ST Aluminum Alloy
• Supplement to Comparison of Automatic Control Systems
• Spin Tests of Two Models of a Low-Wing Monoplane to Investigate Scale Effect in the Model Test Range