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- Calibrations of Service Pitot Tubes in the Langley 24-Inch High-Speed Tunnel
- Correlation Tests of the Ditching Behavior of an Army B-24D Airplane and a 1/16-Size Model
- Airscrew Gyroscopic Moments
- An Investigation of Cowl-Flap and Cowl-Outlet Designs for the Boeing B-29 Power-Plant Installation
- Investigation of Ice Formation in the Induction System of an Aircraft Engine 1: Ground Tests
- Investigation of Ice Formation in the Induction System of an Aircraft Engine 2: Flight Tests
- An Investigation of Cowl Inlets for the B-29 Power-Plant Installation
- Flight Measurements by Various Methods of the Drag Characteristics of the XP-51 Airplane
- Flight Investigation to Improve the Dynamic Longitudinal Stability and Control-Feel Characteristics of the P-63A-1 Airplane (AAF No. 42-68889) with Closely Balanced Experimental Elevators
- Flight Investigation of Factors Affecting the Carburetor Ram and Nacelle Drag of an A-26B Airplane
- High-Speed Longitudinal-Stability and Control Characteristics of the Consolidated Vultee Lark Missile as Predicted from Wind-Tunnel Tests (TED No. NACA 2391)
- The High-Speed Characteristics of Several Flaps and Spoilers on the Upper Surface of the Horizontal Stabilizer of a Model of a Radial-Engine Pursuit Airplane
- Measurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit-Type Airplane at Several Values of Mach Number
- Lead Susceptibility of Several Fuels as Determined in an Air-Cooled Aircraft-Engine Cylinder
- Laboratory Investigation of Icing in the Carburetor and Supercharger Inlet Elbow of an Aircraft Engine 6: Effect of Modifications to Fuel-Spray Nozzle on Icing Characteristics
- Laboratory Investigation of Icing in the Carburetor and Supercharger Inlet Elbow of an Aircraft Engine 4: Effect of Throttle Design and Method of Throttle Operation on Induction-System Icing Characteristics
- Langley Full-Scale Tunnel Investigation of a 1/3-Scale Model of the Chance Vought XF5U-1 Airplane
- A Photographic Profile Recorder for Airscrews and Wing Models
- The Supersonic Axial-Flow Compressor
- On the Problem of Stress Corrosion
- Variation with Mach Number of Static and Total Pressures Through Various Screens
- Wind-Tunnel Investigation of the Horizontal Motion of a Wing Near the Ground
- Analysis of Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane
- Evaluation of Gust and Draft Velocities from Flights of P-61c Airplanes within Thunderstorms August 7, 1946 to August 13, 1946 at Orlando, Florida
- Evaluation of Gust and Draft Velocities from Flights of P-61c Airplanes within Thunderstorms 2 - July 9, 1946 to July 11, 1946 at Orlando, Florida
- Investigation of Dive Brakes and a Dive-Recovery Flap on a High-Aspect-Ratio Wing in the Langley 8-Foot High-Speed Tunnel
- Ditching Tests of a 1/9-Size Model of the Army P-38 Airplane in Langley Tank No. 2 and at the Outdoor Catapult
- High-Speed Wind-Tunnel Tests of a Twin-Fuselage Pursuit Airplane
- Hydraulic Characteristics of the NACA Injection Impeller
- Free-Spinning-Tunnel Tests of a 1/26th Scale Model of the Douglas XTB2D-1 Airplane
- Ground-Stand Cooling Investigation of an R-2600-22 Engine in a PBM-3D Nacelle
- Free-Spinning, Longitudinal-Trim, and Tumbling Tests of 1/17.8-Scale Models of the Cornelius XFG-1 Glider
- Flight Measurements of the Directional Stability and Control of a P-51D Airplane with a Horn-Balanced Rudder as Compared with Previously Tested Vertical-Tail Configurations
- Investigation of the Behavior of Thin-Walled Panels with Cutouts
- Jet-boundary and plan-form corrections for partial-span models with reflection-plane, end-plate, or no end-plate in a closed circular wind tunnel
- Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas A-26 Airplane
- Characteristics of a Sealed Internally Balanced Aileron from Tests of a 1/4-Scale Partial-Span Model of the Republic XF-12 Airplane in the Langley 19-Foot Pressure Tunnel
- Effects of Wing Flaps and Wing Duct Inlet on the Lift and Stalling Characteristics of a 1/4-Scale Partial-Span Model of the Republic XF-12 Airplane in the Langley 19-Foot Pressure Tunnel
- Evaluation of Gust and Draft Velocities from Flights of P-61c Airplanes within Thunderstorms. 3 - July 12, 1946 to July 18, 1946 at Orlando, Florida
- Development of Wing Inlets
- Effect of an Auxiliary Belly Fuel Tank on the Low-Speed Static Stability Characteristics of a 1/5-Scale Model of the Grumman XF8F-1 Airplane, TED No. NACA 2384
- Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil Sections
- Method for calculating wing characteristics by lifting-line theory using nonlinear section lift data
- Tank Tests of a 1/7-Size Powered Dynamic Model of the Grumman XJR2F-1 Amphibian: Spray Characteristics, Take-Off and Landing Stability in Smooth Water - Langley Tank Model 212, TED No. NACA 2378
- Tank Tests of an Alternate Hull Form for the Consolidated Vultee PB2Y-3 Airplane
- Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms: August 23, 1946 to September 4, 1946 at Orlando, Florida
- Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms. 4 - July 19, 1946 to July 20, 1946 at Orlando, Florida
- Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms August 21, 1946 to August 22, 1946 at Orlando, Florida
- Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered with Camouflage Paint
- Flight Investigation of Effect of Various Vertical-Tail Modifications on the Directional Stability and Control Characteristics of the P-63A-1 Airplane (AAF No. 42-68889)