TRAIL - Technical Report Archive and Image Library

Wind-Tunnel Tests on a Series of Wing Models Through a Large Angle of Attack Range Part 1: Force Tests

The Cierva "Autogiro" Mark III (British): Armstrong-Siddeley "Genet Major" Engine

Pressure Distribution Over a Thick, Tapered and Twisted Monoplane Wing Model-N.A.C.A. 81-J

Strength of Welded Joints in Tubular Members for Aircraft

Impact Tests on Rubber Compression Springs for Airplane Landing Gears

Load Assumptions for Calculating the Strength of Airplanes

Effects of the End Fixation of Airplane Struts

Flight Tests for the Determination of Static Longitudinal Stability

Balanced and Servo Control Surfaces

Combating Airplane Fires

A Possible Method for Preventing the Autorotation of Airplane Wings

Experimental Investigations Concerning the Limits of Detonation in Gaseous Mixtures: Part 1

Experimental Research on the Friction of Pivots

"Gloster" Metal Construction

Contribution to the Study of Normal Burning in Gaseous Carbureted Mixtures: Part 1

English Airplane Construction

Structural Details of the Giant Dornier Seaplane "Do X."

Structural Details of German Light Airplanes

Göttingen Six-Component Scale Measurements on a Junkers A 35 Airplane Model

Coefficients of Flow of Standard Nozzles

Diesel-Engine Investigations: Ignition-Chamber Engines

Relation Between the Stability Characteristics and the Controllability of German Airplanes

The Relation Between the Tensile Strength and the Hardness of Metals

The Electrodynamometric Balance of the Small Wind Tunnel of the French Service of Aeronautical Research

The Short "Valetta" Commercial Seaplane (British): A High-Wing All-Metal Twin-Float Monoplane

The Wibault 220 R.N. 3 Airplane (French): A Three-Place Observation High-Wing Monoplane

Westland "Wessex" Commercial Airplane (British): A High-Wing Semicantilever Monoplane

The "Potez 39" Observation Airplane (French): An All-Metal High-Wing Two-Seat Monoplane

The "Avro Trainer" Airplane (British): A Training Biplane

The De Havilland "Moth Three" Airplane (British): A High-Wing Commercial Monoplane

The Boundary Layer as a Means of Controlling the Flow of Liquids and Gases

The Farman "F.300" Commercial Airplane (French): A High-Wing Semicantilever Monoplane

The Comper C(La)7 "Swift" Airplane (English): A High-Wing Single-Seat Monoplane

Vickers "Viastra I" Commercial Airplane (British): A High-Wing All-Metal Semicantilever Monoplane

Identification of Aircraft Tubing by Rockwell Test

Static, Drop, and Flight Tests on Musselman Type Airwheels

Aerodynamic Characteristics of Twenty-Four Airfoils at High Speeds

Tests of Five Metal Model Propellers With Various Pitch Distributions in a Free Wind Stream and in Combination With Model VE-7 Fuselage

Annual Report of the National Advisory Committee for Aeronautics (15th). Administrative Report Including Technical Reports Nos. 309 to 336

Fuel Vapor Pressures and the Relation of Vapor Pressure to the Preparation of Fuel for Combustion in Fuel Injection Engines

Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel

Full-scale tests of metal propellers at high tip speeds

Coefficients of discharge of fuel-injection nozzles for compression-ignition engines

Comparative flight performance with an NACA Roots supercharger and a turbocentrifugal supercharger

Comparison of full-scale propellers having R.A.F.-6 and Clark Y airfoil sections

Maneuverability investigation of the F6C-3 airplane with special flight instruments

Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes

Pressure distribution over a symmetrical airfoil section with trailing edge flap

Pressure distribution over the fuselage of a PW-9 pursuit airplane in flight

Maneuverability investigation of an F6C-4 fighting airplane

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