Browse TRAIL Inventories

The "Comte A.C. 3" military airplane (Swiss) : a high-wing semicantilever monoplane

Flow and Force Equations for a Body Revolving in a Fluid

The measurement of fluctuations of air speed by the hot-wire anemometer

The Behm acoustic sounder for airplanes with reference to its accuracy

Pressure element of constant logarithmic stiffness for temperature compensated altimeter

The effect of supercharger capacity on engine and airplane performance

Joint report on standardization tests on N.P.L. R.A.F 15 airfoil model

Collection of wind-tunnel data on commonly used wing sections

Flight tests on U.S.S. Los Angeles. Part 2: stress and strength determination

Dynamic and flight tests on rubber-cord and oleo-rubber-disk landing gears for an F6C-4 airplane

Air forces and air-force moments at large angles of attack and how they are affected by the shape of the wing

Aerodynamic characteristics of airfoils VI : continuation of reports nos. 93, 124, 182, 244, and 286

Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch

A method of flight measurement of spins

Identification of Aircraft Tubing by Rockwell Test

Pressure Fluctuations in a Common-Rail Fuel Injection System

The Pressure Distribution Over the Wings and Tail Surfaces of a PW-9 Pursuit Airplane in Flight

An Investigation of the Effectiveness of Ignition Sparks

The "Junkers-Junior" Light Airplane (German): A Two-Seat All-Metal Low-Wing Cantilever Monoplane

Rolling Moments Due to Rolling and Yaw for Four Wing Models in Rotation

The Junkers "G 38" Commercial Airplane (German): A Giant High-Wing Monoplane

An Extended Theory of Thin Airfoils and Its Application to the Biplane Problem

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


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