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• 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
• Pressure-distribution measurements at large angles of pitch on fins of different span-chord ratio on a 1/40-scale model of the U. S. Airship "Akron"
• Air propellers in yaw
• 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
• An analysis of the factors that determine the periodic twist of an autogiro rotor blade, with a comparison of predicted and measured results
• 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
• Motion of the Two-Control Airplane in Rectilinear Flight After Initial Disturbances With Introduction of Controls Following an Exponential Law
• 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
• The Source of Propeller Noise
• 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
• Helicopter Problems
• Turbulent Boundary Layer of an Airfoil
• Universal Logarithmic Law of Velocity Distribution as Applied to the Investigation of Boundary Layer and Drag of Streamline Bodies at Large Reynolds Number
• Detonation and Autoignition: Some Considerations on Methods of Determination