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A Flight Investigation of Exhaust-Heat De-Icing, Special Report

Investigation of the Boundary Layer About a Symmetrical Airfoil in a Wind Tunnel of Low Turbulence

Flow Around Wings Accompanied by Separation of Vortices

High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane

Full-Scale Tests of 4- and 6-Blade, Single- and Dual-Rotating Propellers, Special Report

Full-Scale Tests of Several Propellers Equipped with Spinners, Cuffs, Airfoil and Round Shanks, and NACA 16-Series Sections, Special Report

Flight Tests of Exhaust-Gas Jet Propulsion

Flight Tests of Exhaust Gas Jet Propulsion, Special Report

Creep Strength of Stabilized Wrought-Aluminum Alloys

Note on the Calculation of Boundary Layers

Constant-Pressure Blowers

Recent Work on Airfoil Theory

High-speed drag tests of several fuselage shapes in combination with a wing

A graphical method of determining pressure distribution in two-dimensional flow

Stresses in Single-Spar Wing Constructions With Incompletely Built-Up Ribs

Drag and propulsive characteristics of air-cooled engine-nacelle installations for two-engine airplanes

Effect of body nose shape on the propulsive efficiency of a propeller

Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel

Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel, Special Report

Investigation of the Characteristics of a High-Aspect-Ratio Wing in the Langley 8-Foot High-Speed Tunnel

Wind tunnel tests of air inlet and outlet openings on a streamline body

Propeller charts for the determination of the rotational speed for the maximum ratio of the propulsive efficiency to the specific fuel consumption

Preliminary Tests in the NACA Tank to Investigate the Fundamental Characteristics of Hydrofoils

Wind-tunnel investigation of an NACA 23012 airfoil with two sizes of balanced split flap

Wind-tunnel investigation of air inlet and outlet openings on a streamline body

Annual Report of the National Advisory Committee for Aeronautics (25th). Administrative Report Including Technical Report Nos. 645 to 680

Analysis of Wind-Tunnel Data on Directional Stability and Control

The Calculated Effect of Various Hydrodynamic and Aerodynamic Factors on the Take-Off of a Large Flying Boat

An Analysis of the Stability of an Airplane With Free Controls

Flow coefficients of monosleeve valves

Determination of ground effect from tests of a glider in towed flight

Determination of the Characteristics of Tapered Wings

A theoretical study of lateral stability with an automatic pilot

A high-speed motion-picture study of normal combustion, knock and preignition in a spark-ignition engines

Propeller analysis from experimental data

Pressure distribution over NACA 23012 airfoil with a slotted and a split flap

Piston temperatures in an air-cooled engine for various operating conditions

Preliminary investigation of the flying qualities of airplanes

Pressure available for cooling with cowling flaps

The Aileron as an Aid to Recovery From the Spin

Analysis of Cylinder-Pressure-Indicator Diagrams Showing Effects of Mixture Strength and Spark Timing

Aerodynamic heating and the deflection of drops by an obstacle in an air stream in relation to aircraft icing

Radiator design

General Airfoil Theory

Some comparative tests of plain and alclad 24S-T sheet

Comparison of stress-strain curves obtained by single-thickness and pack methods

Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with flight tests

Compression tests of some 17S-T aluminum-alloy specimens of I cross section

The effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression

Effect of alternately high and low repeated stresses upon the fatigue strength of 25S-T aluminum alloy


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