Browse TRAIL Inventories

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

The Response of Pressure Measuring Systems to Oscillating Pressures

Notes on the Foundations of the Theory of Small Displacements of Orthotropic Shells

Effect of Automatic Stabilization on the Lateral Oscillatory Stability of a Hypothetical Airplane at Supersonic Speeds

Hydrodynamic Impact Loads in Smooth Water for a Prismatic Float Having an Angle of Dead Rise of 40 Degrees

Critical Combinations of Shear and Direct Axial Stress for Curved Rectangular Panels

Wind-Tunnel Investigation of an NACA 65-210 Semispan Wing Equipped With Circular Plug Ailerons and a Full-Span Slotted Flap

Theory of the Inlet and Exhaust Processes of Internal-Combustion Engines

Summary of Information Relating to Gust Loads on Airplanes

A Rapid Graphical Method for Computing the Pressure Distribution at Supersonic Speeds on a Slender Arbitrary Body of Revolution

On Compressibility Corrections for Subsonic Flow Over Bodies of Revolution

Observations on the Maximum Average Stress of Flat Plates Buckled in Edge Compression


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