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Test-Stand Investigation of Cooling Characteristics and Factors Affecting Temperature Distribution of a Double-Row Aircraft Engine

Tests of a 1/7-Scale Powered Model of the Kaiser Tailless Airplane in the Langley Full-Scale Tunnel

Tests of Cast Aluminum-Alloy Mixed-Flow Impellers

The Influence of the Jet of a Propulsion Unit on Nearby Wings

Investigation of Flow in a Centrifugal Pump

Investigation of Turbulent Mixing Processes

The Effect on the Sperry Directional Gyro in Turning

Flight Measurements to Determine Effect of a Spring-Loaded Tab on Longitudinal Stability of an Airplane

Flow Investigation With the Aid of the Ultramicroscope

The Further Development of Heat-Resistant Materials for Aircraft Engines

Investigations of Pressure Distribution on Fast Flying Bodies

Correlation of Mixture Temperature Data Obtained From Bare Intake-Manifold Thermocouples

The Effect of Liquid and Ice Particles on the Erosion of a Supercharger-Inlet Cover and Diffuser Vanes

Efficiency of a Radial-Flow Exhaust-Gas Turbosupercharger Turbine With a 12.75-Inch Tip Diameter

An Evaluation of the Knock-Limited Performance of Triptane

Experimental Determination of the Effect of Negative Dihedral on Lateral Stability and Control Characteristics at High Lift Coefficients

Annual Report of the National Advisory Committee for Aeronautics (28th). Administrative Report Including Technical Report Nos. 727 to 751

The Effect of Increase in Combustion-Air Inlet Temperature From 80 to 130 F on the Sea-Level Performance of a 22-Inch-Diameter Pulse-Jet Engine

Effects of Fuel-Vapor Loss on Knock-Limited Performance and Inspection Properties of Aviation Fuels

The Effect of Ethylene Dibromide on the Knock-Limited Performance of Leaded and Nonleaded S Reference Fuel

Determination of Towline Tension and Stability of Spin-Recovery Parachutes

An Investigation of the Icing and Heated-Air De-Icing Characteristics of the R-2600-13 Induction System

Performance of the Modified V-1710-93 Engine-Stage Supercharger with a Constant-Area Vaneless Diffuser

Performance of the 19XB 10-Stage Axial-Flow Compressor

Aerodynamic Characteristics of Several Modifications of a 0.45-Scale Model of the Vertical Tail of the Curtiss XP-62 Airplane

Aerodynamic Data for a Wing Section of the Republic XF-12 Airplane Equipped With a Double Slotted Flap

Aerodynamic Characteristics of Four NACA Airfoil Sections Designed for Helicopter Rotor Blades

Analysis of V-G Records from the SNB-1 Airplane

Effect of Three Modifications on Performance of Auxiliary-Stage Supercharger for V-1710-93 Engine

Free-Spinning-Tunnel Tests of a 1/18-Scale Model of the Fairchild XNQ-1 Airplane, TED No. NACA 2398

Performance of 19XB-2A Gas Turbine 1 - Effect of Pressure Ratio and Inlet Pressure on Turbine Performance for an Inlet Temperature of 800 Degrees R

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 14S-T Aluminum Alloy

Compressibility Effects on the Longitudinal Stability and Control of a Pursuit-Type Airplane as Measured in Flight

Altitude-Wind-Tunnel Investigation of Oil-System Performance of XR-4360-8 Engine in XTB2D-1 Airplane

Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 4 - Curtiss 732-1C2-0 Four-Blade Propeller

Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loading 2 - Curtiss 838-1C2-18R1 Four-Blade Propeller

Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 6 - Hamilton Standard 6507A-2 Four- and Three-Blade Propellers

Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 5 - Curtiss 836-14C2-18R1 Four-Blade Propeller

Calibration Tunnel for High Speed

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)


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