Browse TRAIL Inventories

A Method of Determining the Equilibrium Performance and the Stability of an Engine Equipped With an Exhaust Turbosupercharger

The theoretical lateral motions of an automatically controlled airplane subjected to a yawing moment disturbance

Hydrodynamic Tests of a 1/10-Size Model of the Hull of the Latécoère 521 Flying Boat: NACA Model 83

The Effects of Aerodynamic Heating on Ice Formations on Airplane Propellers

Effect of several supercharger control methods on engine performance

Velocity gained and altitude lost in recoveries from inclined flight paths

Wind-tunnel investigation of effect of yaw on lateral-stability characteristics 3: symmetrically tapered wing at various positions on circular fuselage with and without a vertical tail

Critical Compressive Stress for Flat Rectangular Plates Supported Along all Edges and Elastically Restrained Against Rotation Along the Unloaded Edges

Potential Flow Through Centrifugal Pumps and Turbines

Preliminary Report on Flight Tests of an Airplane Having Exhaust-Heated Wings

Tables for Computing Various Cases of Beam Columns

A Remote Indicating Hinge-Moment Balance, Special Report

Restraint Provided a Flat Rectangular Plate by a Sturdy Stiffener Along an Edge of the Plate, Special Report

Propeller-Design Problems of High-Speed Airplanes, Special Report

Wind-Tunnel Investigation of a Plain and Slot-Lip Aileron on a Wing With a Full-Span Slotted Flap

Wind-Tunnel Investigation of a Spoiler-Slot Aileron on an NACA 23012 Airfoil With a Full-Span Fowler Flap

Wind-Tunnel Investigation of an NACA 66,2-216 Low-Drag Wing with Split Flaps of Various Sizes, Special Report

Wind-Tunnel Investigation of an NACA Low-Drag Tapered Wing With Straight Trailing Edge and Simple Split Flaps, Special Report

Wind-Tunnel Investigation of an NACA 23012 Airfoil With 30 Percent-Chord Venetian-Blind Flaps

Two-Dimensional Potential Flow Past a Smooth Wall With Partly Constant Curvature

Lift and Drag Characteristics of a Low-Drag Airfoil With Slotted Flap Submitted by Curtiss-Wright Corporation

Pressure-Distribution Measurements of a Low-Drag Airfoil With Slotted Flap Submitted by Curtiss-Wright Corporation

Wind-Tunnel Tests of Several Model Tractor-Propeller and Pusher-Propeller Wing Extension-Shaft Arrangements, Special Report

Tests of Wing Machine-Gun and Cannon Installations in the NACA Full-Scale Wind Tunnel, Special Report

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

Effects of Some Present-Day Airplane Design Trends on Requirements for Lateral Stability

Comparison of Vee-Type and Conventional Tail Surfaces in Combination with Fuselage and Wing in the Variable-Density Tunnel

Determination of the Bending and Buckling Effect in the Stress Analysis of Shell Structures Accessible From One Side Only

General Airfoil Theory

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


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