Browse TRAIL Inventories

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

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

Experimental Determination of Exhaust Gas Thrust, Special Report

The Effect of Initial Displacement of the Center Support on the Buckling of a Column Continuous Over Three Supports

The Effects of Aerodynamic Heating on Ice Formations on Airplane Propellers

New Equipment for Testing the Fatigue Strength of Riveted and Welded Joints

Comparison of Three Exit-Area Control Devices on an N.A.C.A. Cowling, Special Report

Consideration of Auxiliary Jet Propulsion for Assisting Take-Off

The Maximum Delivery Pressure of Single-Stage Radial Superchargers for Aircraft Engines

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

Design of nozzles for the individual cylinder exhaust jet propulsion system

Determination of control-surface characteristics from NACA plain-flap and tab data

Statistical analysis of the time and fatigue strength of aircraft wing structures

The effects of hub drag, solidity, dual rotation, and number of blades upon the efficiency of high-pitch propellers

Tail-load measurements on the XB-15 bomber in gusty air

Additional power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps

Effect of humidity on several supercharger parameters

Investigation of performance of 9-cylinder engine using large valve overlap and eclipse fuel-injection system


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