Search U.S. government technical reports digitized or harvested by TRAIL.
Data on the Design of Plywood for Aircraft
Moisture Resistant Finishes for Airplane Woods
Tin Soldering of Aluminum and Its Alloys
N.A.C.A. Langley field wind tunnel apparatus: The tilting manometer
N.A.C.A. Recording Air Speed Meter
The 300 H.P. Benz Aircraft Engine
The 1000 HP Traffic Airplane of the Zeppelin Works in Staaken
Airplane Crashes: Engine Troubles: A Possible Explanation
The Effect of the Nature of Surfaces on Resistance as Tested on Struts
Causes of cracking of ignition cable
Crippling Strength of Axially Loaded Rods
Loads and Calculations of Army Airplanes
The Choice of Wing Sections for Airplanes
Effects of Varying the Relative Vertical Position of Wing and Fuselage
A Mechanical Device for Illustrating Airplane Stability
Aneroid investigations in Germany
Mutual Influence of Wings and Propeller
An Investigation on the Effect of Raked Wing Tips
Performance of a vane driven-gear pump
Similitude tests on wing sections
A New Method of Testing in Wind Tunnels
Recent European Developments in Helicopters
The Factors That Determine the Minimum Speed of an Airplane
Gordon Bennett Airplane Cup 1920
On the Resistance of the Air at High Speeds and on the Automatic Rotation of Projectiles
Absolute Coefficients and the Graphical Representation of Aerofoil Characteristics
The development of German Army airplanes during the war
The Dynamometer Hub for the Testing Propellers and Engines During Flight
Influence of Span and Load Per Square Meter on the Air Forces of the Supporting Surface
The determination of the effective resistance of a spindle supporting a model aerofoil
Effect of the Reversal of Air Flow Upon the Discharge Coefficient of Durley Orifices
The optical wing aligning device of the Langley Field tunnel
The Effect of Staggering a Biplane
Experiments With Slotted Wings
Langley Field wind tunnel apparatus
Vortices and the Related Principles of Hydrodynamics
The Problem of Fuel for Aviation Engines
Effect of the Reversal of Air Flow Upon the Discharge Coefficient of Durley Orifices