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• An Analytical Investigation of the Effects of Elevator-Fabric Distortion on the Longitudinal Stability and Control of an Airplane
• An Automatically Variable Control Linkage and Its Effect on the Lateral-Control Characteristics of a High-Speed Fighter Airplane
• Charts Showing Stability and Control Characteristics of Airplanes in Flight
• Comparative Tests of the Strength and Tightness of Commercial Flush Rivets of One Type and NACA Flush Rivets in Machine-Countersunk and Counterpunched Joints
• Comparative Cooling of Cylinders of Nonuniform Fin Width With Tight-Fitting Baffles and With Baffles That Provide Constant Flow-Path Areas
• Compression Tests of Six Curved Paper-Base Plastic Panels With Outward-Acting Normal Pressure
• Collection of Balanced-Aileron Test Data
• Comparison of Yaw Characteristics of a Single-Engine Airplane Model With Single-Rotating and Dual-Rotating Propellers
• Compressive Strength of Flat Panels With Z-Section Stiffeners
• Compressive Strength of Corrugated-Sheet-Stiffened Panels for Consolidated XB-36 Airplane
• Calculation of Stick Forces for an Elevator With a Spring Tab
• Calculations of Intake-Air Cooling Resulting From Water Injection and of Water Recovery From Exhaust Gas
• Continuous Use of Internal Cooling to Suppress Knock in Aircraft Engines Cruising at High Power
• Axial Superchargers
• Analysis of Experimental Investigations of the Planing Process of the Surface of Water
• Maximum Rates of Control Motion Obtained From Ground Tests
• Maximum Lift Coefficients of Airplanes Based on Sum of Wing and Tail Areas
• Material Properties of Two Types of Plastic-Bonded Glass Cloth
• Investigation of Single Stage Axial Fans
• Method of Mounting Cylinder Blocks of in-Line Engines on CUE Crankcases
• The NACA Impact Basin and Water Landing Tests of a Float Model at Various Velocities and Weights
• The NACA Balanced-Diaphragm Dynamometer-Torque Indicator
• Heat-Capacity Lag in Turbine-Working Fluids
• An Investigation of the Mutual Interference Effects of a Tail-Surface: Stern Propeller Installation on a Model Simulating the Douglas XB-42 Empennage
• Knock-Limited Blending Characteristics of Blends of Triptane and 28-R Aviation Fuel
• Knock-Limited Performance of Pure Hydrocarbons Blended With a Base Fuel in a Full-Scale Aircraft-Engine Cylinder 1: Eight Paraffins, Two Olefins
• The Low-Temperature Solubility of 24 Aromatic Amines in Aviation Gasoline
• The Low-Temperature Solubility of Aniline, the Toluidines and Some of Their N-Alkyl Derivatives in Aviation Gasoline
• Measurement of Flying Qualities of a Douglas A-26B Airplane (AAF No. 41-39120) 1: Longitudinal Stability and Control Characteristics
• Measurements in Flight of the Lateral-Control Characteristics of an Airplane Equipped with Full-Span Zap Flaps and Simple Circular-Arc-Type Ailerons
• NACA Investigation of a Jet-Propulsion System Applicable to Flight
• The NACA Impact Basin and Water Landing Tests of a Float Model at Various Velocities and Weights
• An Investigation of the Characteristics of a Propeller Alcohol Feed Ring
• Knock-Limited Performance of Blends of AN-F-28 Fuel Containing 2 Percent Aromatic Amines 4
• A Laboratory Investigation of Icing and Heated-Air De-Icing of a Chandler-Evans 1900 CPB-3 Carburetor Mounted on a Pratt and Whitney R-1830-C4 Intermediate Rear Engine Section
• The Knock-Limited Performance of Several Fuels Blended With S-2 Reference Fuel
• Landing Characteristics of a Model of a Flying Boat With the Depth of Step Reduced to Zero by Means of a Retractable Planing Flap
• The Landing Stability of a Powered Dynamic Model of a Flying Boat With a 30 Degree V-Step and With Two Depths of Transverse Step
• Some Notes on the Determination of the Stick-Free Neutral Point from Wind-Tunnel Data
• The Surface Structure of Ground Metal Crystals
• Methods of Stress Calculation in Rotating Disks
• The Wall Interference of a Wind Tunnel of Elliptic Cross Section
• The Theory of a Free Jet of a Compressible Gas
• Application of Spring Tabs to Elevator Controls
• Accelerations Measured at Center of Gravity and Along Span of the Wing of a B-24D Airplane in Landing Impacts
• Aerodynamic Tests of an NACA 66(215)-116, a=0.6 Airfoil With a 0.25c Slotted Flap for the Fleetwings XA-39 Airplane
• Detail Calculations of the Estimated Shift in Stick-Fixed Neutral Point Due to the Windmilling Propeller and to the Fuselage of the Republic XF-12 Airplane
• High-Speed Wind-Tunnel Tests of Semispan Horizontal Tails With Fabric-Covered and Metal-Covered Elevators for a Bomber Airplane
• Flight Variables Affecting Fuel-Vapor Loss From a Fuel Tank
• Flying Qualities of a High-Speed Bomber With a Dual Pusher Propeller Aft of the Empennage as Estimated From Wind-Tunnel Tests of a 1/8-Scale Powered Model