Browse TRAIL Inventories

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


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