Search U.S. government technical reports digitized or harvested by TRAIL.
The Variation in Pressures in the Cockpit Fan Airplane in Flight
The Reaction on a Float Bottom When Making Contact With Water at High Speeds
The Drag of a J-5 Radial Air-Cooled Engine
Preliminary biplane tests in the variable density wind tunnel
A Dangerous Seaplane Landing Condition
The Effect of the Sperry Messenger Fuselage on the Air Flow at the Propeller Plane
Determination of Propeller Deflection by Means of Static Load Tests on Models
Pressure distribution on wing ribs of the VE-7 and TS airplanes in flight Part 2: pull-ups
Drag of exposed fittings and surface irregularities on airplane fuselages
Resistance of streamline wires
A Comparison of Propeller and Centrifugal Fans for Circulating the Air in a Wind Tunnel
An automatic speed control for wind tunnels
The 1926 German Seaplane Contest
Force Measurements on Airplanes
Impact waves and detonation. Part II
Aerodynamic theory and tests of strut forms. Part II
Forces on elliptic cylinders in uniform air stream
Reduction of observed airplane performance to standard conditions
Investigation of damping liquids for aircraft instruments
Fire prevention on airplanes. Part I
Fire prevention on airplanes. Part II
Technical report of the 1928 Rhon soaring-flight contest
Nieuport-Delage 640 (French) : commercial high-wing monoplane
The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine
The Blackburn "Bluebird" Mark IV (British) all-metal biplane
The Bernard 20 C.1 (French) : a single-seat pursuit monoplane
Torsional Rigidity of Cantilever Wings With Constant Spar and Rib Sections
Impact Waves and Detonation: Part 1
Landing and Braking of Airplanes
Remarks on Airplane Struts and Girders Under Compressive and Bending Stresses: Index Values
On the Strength of Box Type Fuselages
Effect of Oxygen on the Ignition of Liquid Fuels
Experiments With a Wing Model From Which the Boundary Is Removed by Suction
Full-Scale Wind-Tunnel Tests on Several Metal Propellers Having Different Blade Forms
Full-Scale Wind-Tunnel Tests With a Series of Propellers of Different Diameters on a Single Fuselage
The Gaseous Explosive Reaction at Constant Pressure: The Reaction Order and Reaction Rate