Search U.S. government technical reports digitized or harvested by TRAIL.
Wind-Tunnel Investigation of Carburetor-Air Inlets
Theory of Heat Transfer and Hydraulic Resistance of Oil Radiators
Influence of Loading Condition on Piloting Technique for Spin Recovery for Pursuit Airplanes
The Influence of Bulkhead Spacing on Bending Stresses Due to Torsion
Pressure-Drop Characteristics of Orifice Plates Used to Simulate Radiators
The Strength and Stiffness of Shear Webs With Round Lightening Holes Having 45 Degree Flanges
A Preliminary Investigation of the Characteristics of Air Scoops on a Fuselage
On a New Method for Calculating the Potential Flow Past a Body of Revolution
The Stresses in Stiffener Openings
A Study of the Tightness and Flushness of Machine-Countersunk Rivets for Aircraft
Wind Tunnel Tests of Wickwire-Spencer Propeller
Investigation of Drag and Pressure Distribution of Windshields at High Speeds
Diagrams for Calculation of Airfoil Lattices
Test of a Dual-Rotation Axial-Flow Fan
Performance Characteristics of Mixed-Flow Impeller and Vaned Diffuser With Several Modifications
Pressure Distribution on Wings in Reversed Flow
Electrical Equipment for the Experimental Study of the Dynamics of Fluids
Recording Rapidly Changing Cylinder-Wall Temperatures
Calibration of Three Temperature Probes and a Pressure Probe at High Speeds
Cooling Investigation of a B-24D Engine-Nacelle Installation in the NACA Full-Scale Tunnel
Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models
Tests of a Large Spherical Turret and a Modified Turret on a Typical Bomber Fuselage
Control of Torsional Vibrations by Pendulum Masses
Effect of Normal Pressure on the Critical Compressive Stress of Curved Sheet
The Influence of Impact Velocity on the Tensile Characteristics of Some Aircraft Metals and Alloys
Square Plate With Clamped Edges Under Normal Pressure Producing Large Deflections
On a New Method for Calculating the Potential Flow Past a Body of Revolution
Experimental Investigation of a New Type of Low-Drag Wing-Nacelle Combination
Tests of a Heated Low-Drag Airfoil
Bending of Rectangular Plates with Large Deflections
Preliminary Low-Drag-Airfoil and Flap Data from Tests at Large Reynolds Numbers and Low Turbulence
The Effect of Valve Cooling Upon Maximum Permissible Engine Output as Limited by Knock
Torsion Tests of a Monocoque Box
Results of landing tests of various airplanes
A study of general instability of box beams with truss-type ribs