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- Effect of NACA Injection Impeller on Mixture Distribution of Double-Row Radial Aircraft Engine
- The Effect of Six Aromatic Amines on the Preignition-Limited Performance of 28-R Aviation Fuel in a CFR Engine
- The Effect of Valve Clearance on Knock-Limited Performance and Engine Cooling
- The Effect of the Skis on the Power-Off Stability Characteristics of a Twin-Engine Cargo Airplane
- Effects of Compressibility and Large Angles of Yaw on Pressure Indicated by a Total-Pressure Tube
- Effect of Engine-Operating Variables and Internal Coolants on Spark-Advance Requirements of a Liquid-Cooled Cylinder
- The Effect of Compression Ratio on Knock Limits of High-Performance Fuels in a CFR Engine 3: Blends of 2,3-Dimethylpentane With 28-R
- Effect of Fuel Volatility and Mixture Temperature on the Knocking Characteristics of a Liquid-Cooled Single-Cylinder Test Engine
- Determination of Air-Consumption Parameters for Two Radial Aircraft Engines
- Determination From Flight Tests of Thrust Coefficients for 10 Full-Scale Airplanes in the Gliding Condition With Engine Idling
- Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-Flight Tunnel
- Dilution of Exhaust-Gas Samples From a Multicylinder Engine Equipped With an Exhaust-Gas Collector
- The Effect of High-Resistance Ignition Cable on the Erosion of Spark-Plug Electrodes
- An Analysis of the Dissipation of Heat in Conditions of Icing From a Section of the Wing of the C-46 Airplane
- An Analysis of Jet-Propulsion Systems Making Direct Use of the Working Substance of a Thermodynamic Cycle
- Aerodynamic Characteristics of Four Republic Airfoil Sections from Tests in Langley Two-Dimensional Low-Turbulence Tunnels
- Charts for the Minimum-Weight Design of 24S-T Aluminum-Alloy Flat Compression Panels With Longitudinal Z-Section Stiffeners
- Attainment of a Straight-Line Trajectory for a Preset Guided Missile With Special Reference to Effect of Wind or Target Motion
- Comparison of the Knock-Limited Performance of Triptane With 23 Other Purified Hydrocarbons
- Comparison of Structural Efficiencies of Diagonal-Tension Webs and Truss Webs of 24S-T Aluminum Alloy
- Column and Plate Compressive Strengths of Aircraft Structural Materials: 24S-T Aluminum-Alloy Sheet
- A Comparison of Data Obtained by Two Flight Techniques for Determining the Sideslip Characteristics of a Fighter Airplane
- Comparison of Predicted and Actual Control-Fixed Stability and Control Characteristics of a Douglas A-26B Airplane
- Control of Cylinder Temperatures by Thermostatically Operated Internal-Coolant Valves
- Correlation of the Characteristics of Single-Cylinder and Flight Engines in Tests of High-Performance Fuels in an Air-Cooled Engine 1 - Cooling Characteristics
- Computation of the Mean Tangential Velocity of the Air Leaving the Blade Tips of a Centrifugal Supercharger
- Cooling of a Double-Row Radial Engine by Water Injection to the Individual Cylinders
- Calculation of the Aileron and Elevator Stick Forces and Rudder Pedal Forces for the Bell XP-83 Airplane (Project MX-511) in Spins
- Characteristics of Several Single- and Dual-Rotating Propellers in Negative Thrust
- Characteristics of the BMW 801D2 Automatic Engine Control as Determined From Bench Tests
- Calculations of Economy of 18-Cylinder Radial Aircraft Engine With Exhaust-Gas Turbine Geared to the Crankshaft
- Correlation of the Characteristics of Single-Cylinder and Flight Engines in Tests of High-Performance Fuels in an Air-Cooled Engine 2 - Knock-Limited Charge-Air Flow and Cylinder Temperatures
- Correlation of Wind-Tunnel Predictions With Flight Tests of a Twin-Engine Airplane 1: Longitudinal-Stability and -Control Characteristics
- Correlation of Wind-Tunnel Predictions With Flight Tests of a Twin-Engine Patrol Airplane 2: Lateral- and Directional-Stability and Control Characteristics
- Wind-Tunnel Tests of a 1/6-Scale Model of Republic XF-12 Vertical Tail with Stub Fuselage and Stub Horizontal Tail
- Analysis of V-G Records From the SNJ-4 Airplane
- An Approximate Determination of the Power Required to Move Control Surfaces as Related to Control-Booster Design
- Measurement of Individual Aileron Hinge Moments and Aileron Control Characteristics of a P-40F Airplane
- A Method for Correlating the Cooling Data of Liquid-Cooled Engines and Its Application to the Allison V-3420-11 Engine
- Longitudinal-Trim Tests of a 0.059-Scale Model of the Curtiss-Wright XP-55 Airplane
- Investigation of Slipstream Effects on a Wing-Inlet Oil-Cooler Ducting System of a Twin-Engine Airplane in the Ames 40- by 80-Foot Wind Tunnel
- An Investigation of Backflow Phenomenon in Centrifugal Compressors
- A Method for the Determination of Aromatics in Hydrocarbon Mixtures
- Flight Investigation of the Variation of Drag Coefficient With Mach Number for the Bell P-39N-1 Airplane
- A Flight Investigation of the Ice-Prevention Requirements of the United States Naval K-Type Airship
- Flight Investigation of Boundary-Layer and Profile-Drag Characteristics of Smooth Wing Sections of a P-47D Airplane
- Flight Investigation of Modifications to Improve the Elevator Control-Force Characteristics of the Curtiss SB2C-1C Airplane in Maneuvers
- High-Speed Photographs of a YR-4B Production Rotor Blade for Simulated Flight Conditions in the Langley Full-Scale Tunnel
- An Investigation of the Ranger V-770-8 Engine Installation for the Edo XOSE-1 Airplane 2: Aerodynamics
- Knock-Limited Blending Characteristics of Benzene, Toluene, Mixed Xylenes, and Cumene in an Air-Cooled Cylinder