Search U.S. government technical reports digitized or harvested by TRAIL.
Wake studies of eight model propellers
An electron microscope study of used nitrated-steel piston rings
High-speed investigation of skin wrinkles on two NACA airfoils
Performance of Hoods for Aircraft Exhaust-Gas Turbines
Preliminary Investigation of the Loads Carried by Individual Bolts in Bolted Joints
Tensile Properties of a Sillimanite Refractory at Elevated Temperatures
Strain-Gage Study of Internally Cooled Exhaust Valves Having Various Throat Designs
Stresses Around Large Cut-Outs in Torsion Boxes
The Problem of Noise Reduction With Reference to Light Airplanes
Use of Ducted Head Baffles to Reduce Rear-Row Cylinder Temperatures of an Air-Cooled Aircraft Engine
Investigation of the Stability of the Laminar Boundary Layer
Thermodynamic Charts for the Computation of Combustion and Mixture Temperatures at Constant Pressure
Development of a Protected Air Scoop for the Reduction of Induction-System Icing
Charts for the Rapid Calculation of the Work Required to Compress Dry Air
An Analysis of the Factors Affecting the State of Fuel and Air Mixtures
The Fatigue Characteristics of Bolted Lap Joints of 24S-T Alclad Sheet Materials
Effect of brake forming on the strength of 24S-T aluminum-alloy sheet
Flutter and oscillating air-force calculations for an airfoil in a two-dimensional supersonic flow
Effect of change in cross section upon stress distribution in circular shell-supported frames
Tests of a full-scale horizontal tail surface in the Langley 16-foot high-speed tunnel
Theoretical lift and drag of thin triangular wings at supersonic speeds
Thin oblique airfoils at supersonic speed
Comparison of measured and calculated stresses in built-up beams
An investigation of additional requirements for satisfactory elevator control characteristics
The effect of simulated icing on propeller performance
Wing plan forms for high-speed flight
Boundary-layer-control tests of two wings in the Langley Propeller-Research Tunnel
Calculation of surface temperatures in steady supersonic flight
Bending-Torsion Flutter Calculations Modified by Subsonic Compressibility Corrections
The effects of various parameters on the load at which spray enters the propellers of a flying boat
Increasing the compressive strength of 24S-T aluminum-alloy sheet by flexure rolling