Search U.S. government technical reports digitized or harvested by TRAIL.
Gasoline-water distribution coefficients of 27 aromatic amines
The effect of continuous knock on the endurance of an aircraft engine cylinder
Effect of coaxial lapping of cast-iron piston rings on ring performance
Knock-limited performance of several internal coolants
Knock-limited performance of several internal coolants
The design of the optimum hull for a large long-range flying boat
Preignition-limited performance of several fuels
Airfoil-contour modifications based on (epsilon)-curve method of calculating pressure distribution
Cascade investigation of buckets for a modern aircraft turbosupercharger
Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel
Compressible potential flow with circulation about a circular cylinder
Analysis of a thermal ice-prevention system for wing leading-edge landing-light installations
Analysis of available data on the effectiveness of ailerons without exposed overhang balance
Effect of water injection on knock-limited performance of a V-type 12-cylinder liquid-cooled engine
Artificial aging of riveted joints made in alclad 24S-T sheet using A17S-T, 17S-T, and 24S-T rivets
The numerical solution of compressible fluid flow problems
Guides for preventing buckling in axial fatigue tests of thin sheet-metal specimens
Analysis of square shear web above buckling load
Performance tests of wire strain gages 1: calibration factors in tension
Nondestructive test methods for spot welds in aluminum alloys
Effect of curvature on strength of axially loaded sheet-stringer panels
Bibliography of piston ring lubrication
Determination of stress-strain relations from "offset" yield strength values
Development of detonation detector suitable for use in flight
The shear of aluminum alloy driven rivets as affected by increasing D/t ratios
An automatic electrical analyzer for 45 degree strain-rosette data
Charts for rapid analysis of 45 degree strain-rosette data
Elastic properties of channels with unflanged lightening holes
Power-Off Tests of the Northrop N9M-2 Tailless Airplane in the 40- by 80-Foot Wind Tunnel