Search U.S. government technical reports digitized or harvested by TRAIL.
Limitations of the Pilot in Applying Forces to Airplane Controls
The 5- by 7-meter wind tunnel of the DVL
Influence of Fuel-Oil Temperature on the Combustion in a Prechamber Compression-Ignition Engine
Further Measurements of Normal Accelerations on Racing Airplanes
The sonic altimeter for aircraft
A preliminary study of flame propagation in a spark-ignition engine
The lateral instability of deep rectangular beams
The behavior of thin-will monocoque cylinders under torsional vibration
Hydrodynamic tests in the N.A.C.A. tank of a model of the hull of the Short Calcutta flying boat
Plastics as structural materials for aircraft
Considerations affecting the additional weight required in mass balance of ailerons
Maximum forces applied by pilots to wheel-type controls
The apparent width of the plate in compression
The stress distribution in shell bodies and wings as an equilibrium problem
Experimental investigation of the problem of surface roughness
Fuel spray and flame formation in a compression-ignition engine employing air flow
Aircraft accidents.method of analysis
Blower cooling of finned cylinders
Effect of tip shape and dihedral on lateral-stability characteristics
The effect of turbulence on the drag of flat plates
Alternating-current equipment for the measurement of fluctuations of air speed in turbulent flow
Tests of related forward-camber airfoils in the variable-density wind tunnel
Auto-ignition and combustion of diesel fuel in a constant-volume bomb
Experimental investigation of wind-tunnel interference on the downwash behind an airfoil
Wind-tunnel tests of 10-foot-diameter autogiro rotors
Wind-tunnel and flight tests of slot-lip ailerons
The critical velocity of a body towed by a cable from an airplane
The Effect of Curvature on the Transition From Laminar to Turbulent Boundary Layer
Static Thrust Analysis of the Lifting Airscrew
A Sound Pressure-Level Meter Without Amplification
Pressure Drop in Tubing in Aircraft Instrument Installations
Stability of Structural Members Under Axial Load
Strain Measurements on Small Duralumin Box Beams in Bending
A Study of the Factors Affecting the Range of Airplanes
Pressure Distribution Over a Clark Y-H Airfoil Section With a Split Flap
Increasing the Strength of Aluminum-Alloy Columns by Prestressing
Noise From Propellers With Symmetrical Sections at Zero Blade Angle
Method of Curved Models and Its Application to the Study of Curvilinear Flight of Airships: Part 2
Method of Curved Models and Its Application to the Study of Curvilinear Flight of Airships: Part 1
Research and Design Problems Introduced by Increased Power Output
Experimental Apparatus for the Study of Propellers
Turbulent Boundary Layer of an Airfoil
Detonation and Autoignition: Some Considerations on Methods of Determination