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- Investigation of the Loads on a Conventional Front and Rear Sliding Canopy
- Investigation of the Trim Characteristics of a 1/20-Scale Model of the Fleetwings XBTK-1 Airplane over a Wide Range of Angles of Attack
- Investigation of X24C-2 10-Stage Axial-Flow Compressor 2: Effect of Inlet-Air Pressure and Temperature of Performance
- Investigation of Turbine of Mark 25 Torpedo Power Plant with Five Nozzle Designs
- Preliminary Tests of a Burner for Ram-Jet Applications
- Preliminary Results of an Altitude-Wind-Tunnel Investigation of a TG-100A Gas Turbine-Propeller Engine 4 - Compressor and Turbine Performance Characteristics
- Preliminary Results of an Altitude-Wind-Tunnel Investigation of a TG-100A Gas Turbine-Propeller Engine II - Windmilling Characteristics
- Preliminary Results of an Altitude-Wind-Tunnel Investigation of a TG-100A Gas Turbine-Propeller Engine 5 - Combustion-Chamber Characteristics
- Performance of the 19XB 10-Stage Axial-Flow Compressor with Altered Blade Angles
- Preliminary Results of an Altitude-Wind-Tunnel Investigation of a TG-100A Gas Turbine-Propeller Engine 3 - Pressure and Temperature Distributions
- Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336
- Air-Stream Surveys in the Vicinity of the Tail of a 1/8.33-Scale Powered Model of the Republic XF-12 Airplane
- Aerodynamic Characteristics of a Number of Modified NACA Four-Digit-Series Airfoil Sections
- Flight Measurements of the Flying Qualities of a Lockheed P-80A Airplane (Army No. 44-85099): Lateral- and Directional-Stability and Control Characteristics
- Flight Investigation of the Effects of Ice on an I-16 Jet-Propulsion Engine
- Flight Tests of a Curtiss No. 838-1C2-18 Three-Blade Propeller Having Trailing-Edge Extensions
- Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the McDonnell XP-88 Airplane with a Conventional Tail
- Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the McDonnell XP-88 Airplane with a Vee Tail
- The High-Speed Longitudinal Stability and Control of the Bell P-39N-1 Airplane as Calculated from Propeller-Off Tests of a 0.35-Scale Model
- The High-Speed Longitudinal Stability and Control of the Bell P-39N-1 Airplane as Calculated from Propeller-Off Tests of a 0.35-Scale Model
- High-Speed Aerodynamic Characteristics of a 1/7-Scale Model of the Northrop YB-49 Airplane
- Estimated Flying Qualities of the Martin Model 202 Airplane
- Estimation of the Spin and Recovery Characteristics of the North American XSN2J-1 Airplane
- Free-Spinning and Tumbling Tests of a 1/16-Scale Model of the McDonnell XP-85 Airplane
- Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the Chance Vought XF5U-1 Airplane, TED No. NACA 2349
- Free-Spinning-Tunnel Tests of a 1/35-Scale Model of the Douglas XB-43 Airplane
- Measurements of Atmospheric Turbulence on Seattle-Alaska Airways
- Comparison of Wind-Tunnel Predictions with Flight Measurements of the Longitudinal-Stability and -Control Characteristics of a Douglas BTD-1 Airplane
- Compilation of Test Data on 111 Free-Spinning Airplane Models Tested in the Langley 15-Foot and 20-Foot Free-Spinning Tunnels
- Computed Temperature Distribution and Cooling of Solid Gas-Turbine Blades
- Cooling of Gas Turbines 6 - Computed Temperature Distribution Through Cross Section of Water-Cooled Turbine Blade
- Cyclic Engine Test of Cast Vitallium Turbine Buckets - I
- Calculation of the Pressure Distribution on Bodies of Revolution in the Subsonic Flow of a Gas Part 1 - Axially Symmetrical Flow
- Calculation of Wing Bending Moments and Tail Loads Resulting from the Jettison of Wing Tips During a Symmetrical Pull-Up
- Cooling of Gas Turbines 1 - Effects of Addition of Fins to Blade Tips and Rotor, Admission of Cooling Air Through Part of Nozzles, and Change in Thermal Conductivity of Turbine Components
- The Crystal Structure at Room Temperature of Six Cast Heat-Resisting Alloys
- Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8, and 19XB-1 Jet-Propulsion Engines 2 - Analysis of Turbine Performance of the 19B-8 Engine
- Tuft Studies of the Flow over a Wing at Four Angles of Sweep
- Wind Tunnel Development of Means to Alleviate Buffeting of the North American XP-82 Airplane at High Speeds
- Data Obtained in the Flight Measurements to Determine the Stability and Control Characteristics of a C-54D Airplane (AAF No. 42-72713) and a Summary of the Test Program
- Wind-Tunnel Investigation of a 1/5-Scale Model of the Ryan XF2R Airplane
- An Analysis of the Full-Floating Journal Bearing
- Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance
- Investigation of High-Performance Fuels in Multicylinder and in Single-Cylinder Engines at High and Cruising Engine Speeds
- Investigation of Axial-Flow Fan and Compressor Rotors Designed for Three-Dimensional Flow
- Investigation of Sea-Level Performance of I-16 Turbojet Engine at Zero Ram with XFR-1 Intake Duct Shroud, and Tail Pipe
- Longitudinal Stability and Stalling Characteristics of a 1/8.33-Scale Model of the Republic XF-12 Airplane
- A Low-Speed Investigation of a Fuselage-Side Air Inlet for use at Transonic Flight Speeds
- Knock-Limited Power Outputs from a CFR Engine Using Internal Coolants 3 - Four Alkyl Amines, Three Alkanolamines, Six Amides, and Eight Heterocyclic Compounds
- Langley Full-Scale-Tunnel Investigation of Maximum Lift and Stability Characteristics of an Airplane Having Approximately Triangular Plan Form (DM-1 Glider)