Browse TRAIL Inventories

An NACA Vane-Type Angle-of-Attack Indicator for use at Subsonic and Supersonic Speeds

Sound-level measurements of a light airplane modified to reduce noise reaching the ground

Summary of section data on trailing-edge high-lift devices

A simplified method for the determination and analysis of the neutral-lateral-oscillatory-stability boundary

Resistance and Spray Characteristics of a 1/13-Scale Model of the Consolidated Vultee Skate 7 Seaplane: TED No. NACA DE 338

Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane with Speedpak Attached

Ditching Investigation of a 1/18-Scale Model of the North American B-45 Airplane

Smooth-Water Landing Stability and Rough-Water Landing and Take-Off Behavior of a 1/13-Scale Model of the Consolidated Vultee Skate 7 Seaplane, TED No. NACA DE 338

High-Speed Wind-Tunnel Investigation of the Lateral Stability Characteristics of a 0.10-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE 301

Longitudinal Stability and Control Characteristics of a Semispan Wind-Tunnel Model of the XF7U-1 Airplane and a Comparison with Complete-Model Wind-Tunnel Tests and Semispan-Model Wing-Flow Tests

Dynamics of a turbojet engine considered as a quasi-static system

Altitude-wind-tunnel investigation of J47 turbojet-engine performance

Two-dimensional unsteady lift problems in supersonic flight

Stability derivatives at supersonic speeds of thin rectangular wings with diagonals ahead of tip Mach lines

Attainable circulation about airfoils in cascade

The development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers

Icing-protection requirements for reciprocating-engine induction system

Effects of wing flexibility and variable air lift upon wing bending moment during landing impacts of a small seaplane

Altitude-wind-tunnel investigation of various can-type burners in Bumblebee 18-inch ram jet

Spark ignition of flowing gases I : energies to ignite propane-air mixtures in pressure range of 2 to 4 inches mercury absolute

Appreciation and Prediction of Flying Qualities

The design of low-turbulence wind tunnels

Hovering and Low-Speed Performance and Control Characteristics of the Kaman Helicopter Rotor System as Determined on the Langley Helicopter Tower. TED No. NACA DE 205

Laminar mixing of a compressible fluid

Direct method of design and stress analysis of rotating disks with temperature gradient

A radar method of calibrating airspeed installations on airplanes in maneuvers at high altitudes and at transonic and supersonic speeds

Lecture Series "Boundary Layer Theory". Part I - Laminar Flows, Part 1, Laminar Flows

Boundary Layer Theory, Part 2, Turbulent Flows

An Approximate Method for Calculation of the Laminar Boundary Layer with Suction for Bodies of Arbitrary Shape

Performance of J33 turbojet engine with shaft-power extraction 3: turbine performance

Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles

Airfoil measurements in the DVL high-speed wind tunnel (2.7-meter diameter)

The effect of rate of change of angle of attack on the maximum lift coefficient of a pursuit airplane

Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness

Performance of 24-inch supersonic axial-flow compressor in air 2: performance of compressor rotor at equivalent tip speeds from 800 to 1765 feet per second

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : characteristics at a Mach number of 1.53 including effect of small variations of sweep

Study of the canard configuration with particular reference to transonic flight characteristics and low-speed characteristics at high lift

Effect of screens in wide-angle diffusers

The application of the statistical theory of extreme values to gust-load problems

The effect of the propeller slipstream on the characteristics of submerged inlets

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Investigation of a large-scale model at low speed

Experimental and Theoretical Studies of Area Suction for the Control of the Laminar Boundary Layer on a Porous Bronze NACA 64A010 Airfoil

Moments of Cambered Round Bodies

Investigations Relating to the Extension of Laminar Flow by Means of Boundary-Layer Suction Through Slots

Observations of Icing Conditions Encountered in Flight During 1948

Remarks Concerning the Behavior of the Laminar Boundary Layer in Compressible Flows

Shear Buckling of Infinitely Long Simply Supported Metalite Type Sandwich Plates

Provisional Symbols and Definitions for Aircraft Turbines

Application of Radial-Equilibrium Condition to Axial-Flow Compressor and Turbine Design

The Buckling of Parallel Simply Supported Tension and Compression Members Connected by Elastic Deflectional Springs


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