Search U.S. government technical reports digitized or harvested by TRAIL.
The Effect of Wind Tunnel Turbulence Upon the Forces Measured on Models
The Induction Factor Used for Computing the Rolling Moment Due to the Ailerons
Structural Weight of Aircraft as Affected by the System of Design
The Testing of Aviation Engines Under Approximate Altitude Conditions
Tests on Duralumin Columns for Aircraft Construction
Nonmetallic diaphragms for instruments
Interference tests on NACA pitot tubes
Flame speed and spark intensity
Air forces on airfoils moving faster than sound
Aerodynamic characteristics of airfoils at high speeds
Standardization tests of NACA no. 1 wind tunnel
Altitude of equilibrium of an airship
Preliminary investigation of the effect of a rotating cylinder in a wing
The effects of shielding the tips of airfoils
The application of propeller test data to design and performance calculations
The sparking voltage of spark plugs
Recent experiments at the Gottingen Aerodynamic Institute
Charts for graphical estimation of airplane performance
Note on the Air Forces on a Wing Caused by Pitching.
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
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
Computation of Cantilever Airplane Wings
Pressure Distribution Over the Wings of an MB-3 Airplane in Flight
Calculation of Wing Spars of Variable Cross-Section and Linear Load