Search U.S. government technical reports digitized or harvested by TRAIL.
Effect of normal pressure on the critical compressive and shear stress of curved sheet
Bending-Torsion Flutter Calculations Modified by Subsonic Compressibility Corrections
Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound
The Use of Geared Spring Tabs for Elevator Control
Visual Studies of Cylinder Lubrication [Part] 1: The Lubrication of the Piston Skirt
An Investigation of Aircraft Heaters 18: A Design Manual for Exhaust Gas and Air Heat Exchangers
The Knock-Limited Performance of S Reference Fuel Plus 2 Milliliters of Triethylthallium Per Gallon
The development and application of high-critical-speed nose inlets
Analysis and modification of theory for impact of seaplanes on water
An Analytical Investigation of the Heat Losses from a U.S. Navy K-Type Airship
Plane and Three-Dimensional Flow at High Subsonic Speeds
Paths of Target Seeking Missiles in Two Dimensions
Wind-Tunnel Investigation of the Stability of the Jettisonable Nose Section of the X-3 Airplane
The infrared spectra of spiropentane methylenecyclobutane and 2-methyl-1-butene
A method for the determination of air infiltration rates in airplane cabins
Performance tests of wire strain gages 4: axial and transverse sensitivities
A preliminary study of a propeller powered by gas jets issuing from the blade tips
The effect of engine variables on the prediction-limited performance of three fuels
Evaluation of two high-carbon precision-cast alloys at 1700 and 1800 F by the rupture test
Effect of misalignment of strain-gage components of strain rosettes
Effect of normal pressure on strength of axially loaded sheet-stringer panels
Steady- and intermittent-flow coefficients of poppet intake valves
The shearing rigidity of curved panels under compression
The synthesis and purification of aromatic hydrocarbons II : 1, 2, 4-trimethylbenzene
The synthesis and purification of aromatic hydrocarbons V : 1-ethyl-3-methylbenzene
Tail-design requirements for satisfactory spin recovery
Strain measurements and strength tests of 25-inch diagonal-tension beams of 75S-T aluminum alloy
Analysis of propeller efficiency losses associated with heated-air thermal de-icing