Search U.S. government technical reports digitized or harvested by TRAIL.
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
Calculation of Tapered Monoplane Wings
Calculation of Pressure Distribution on Airship Hulls
Experimental Investigations Concerning the Limits of Detonation in Gaseous Mixtures: Part 2
Determination of the Best Cross Section for a Box Beam Subjected to Bending Stresses
Contribution to the Theory of Propeller Vibrations
Development of the Junkers-Diesel Aircraft Engine
Experimental Investigation of Aircraft Propellers Exposed to Oblique Air Currents
Practical Tests With The "Auto Control Slot" Part 2: Discussion
Theory of the Landing Impact of Seaplanes
Ratier Metal Propeller With Pitch Variable in Flight
Practical Tests With The "Auto Control Slot" Part 1: Lecture
Contribution to the Study of Normal Burning in Gaseous Carbureted Mixtures: Part 2
The Magnus Effect in Theory and in Reality
Recent Tests of Tailless Airplanes
Present Status of Aircraft Instruments
The Breguet 270 General-Purpose Military Airplane (French): A Two-Seat All-Steel Sesquiplane
The Weymann-Lepère W.E.L. 10 Observation Airplane (French): A High-Wing Monoplane
Measurement of Profile Drag on an Airplane in Flight by the Momentum Method: Part 2
Measurement of Profile Drag on an Airplane in Flight by the Momentum Method: Part 1
The 1929 Rhon soaring-flight contest
Bending Tests of Metal Monocoque Fuselage Construction
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
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
The Design of Airplane Wing Ribs
Elastic Instability of Members Having Sections Common in Aircraft Construction