Search U.S. government technical reports digitized or harvested by TRAIL.
Pressure Distribution on Fuselage of Airplane Model
Recent Progress in the Theoretical Deduction of Airplane Wings
High Velocity Wind Tunnels: Their Application to Ballistics, Aerodynamics, and Aeronautics
Some Problems on the Lift and Rolling Moment of Airplane Wings
Investigation of Slipstream Velocity
Relation Of "Lilienthal Effect" to Dynamic Soaring Flight
The Problem of Fuel Measurement: The Schiske "Konsummeter"
The Effect of Changes in Compression Ratio Upon Engine Performance
European Commercial Aeronautics
Alloys Similar to Duralumin Made in Other Countries Than Germany
Potential Flow in Engine Valves
Light Airplanes of France, Germany, Italy, Belgium, Holland, Czechoslovakia and Lithuania
Effect of Speed on Economy of Airship Traffic
Model Tests With a Systematic Series of 27 Wing Sections at Full Reynolds Number
Increasing the Power of Internal Combustion Engines
Correcting Horsepower Measurements to a Standard Temperature
Determination and Classification of the Aerodynamic Properties of Wing Sections
Results of Recent Experiments With Slotted Wings
Experimental Determination of Pressure Drop Caused by Wire Gauze in an Air Stream
Royal Aero Club Light Aeroplane Competition
A Method for the Direct Determination of Wing-Section Drag
The "Magnus Effect" - the Principle of the Flettner Rotor
Comparison of Model Propeller Tests With Airfoil Theory
Hesselman Heavy-Oil High-Compression Engine
Characteristics of a single float seaplane during take-off
The Reduction of Airplane Flight Test Data to Standard Atmosphere Conditions
Aerodynamic Characteristics of Aircraft With Reference to Their Use
Air Flow Investigation for Location of Angle of Attack Head on a JN4h Airplane
An Altitude Chamber for the Study and Calibration of Aeronautical Instruments
Simplified Propeller Design for Low-Powered Airplanes
Note on the Katzmayr Effect on Airfoil Drag
Discharge Characteristics of a High Speed Fuel Injection System
The comparison of well-known and new wing sections tested in the variable density wind tunnel
The Calculation of Wing Float Displacement in Single-Float Seaplanes
The Estimation of Airplane Performance From Wind Tunnel Tests on Conventional Airplane Models
Model Tests on the Economy and Effectiveness of Helicopter Propellers
Pressure Distribution on the Nose of an Airship in Circling Flight
Determination of the Lift and Drag Characteristics of an Airplane in Flight