Browse TRAIL Inventories

Two-Dimensional Motion of a Gas at Large Supersonic Velocities

Wind-Tunnel Tests on Various Types of Dive Brakes Mounted in Proximity of the Leading Edge of the Wing

Test Report on Three- and Six-Component Measurements on a Series of Tapered Wings of Small Aspect Ratio (Partial Report: Trapezoidal Wing)

Flow Pattern in a Converging-Diverging Nozzle

Lame's Wave Functions of the Ellipsoid of Revolution

Flight Investigation of 6.25-Inch-Diameter Deacon Rocket and 10-Inch-Scale Model Rocket

Some New Problems on Shells and Thin Structures

Spin and Recovery Characteristics of the Northrop XF-89 Airplane

The Static-Pressure Error of a Wing Airspeed Installation of the McDonnell XF-88 Airplane in Dives to Transonic Speeds

Investigation in Simulated Vertical Descent of the Characteristics of a Cargo-Dropping Device having Extensible Rotating Blades

Investigation of a Systematic Group of NACA 1-Series Cowlings With and Without Spinners

Recommendations for Numerical Solution of Reinforced-Panel and Fuselage-Ring Problems

Aerodynamic Characteristics of a 0.5-Scale Model of the Fairchild XSAM-N-2 Lark Missile at High Subsonic Speeds

Response of a Rotating Propeller to Aerodynamic Excitation

Experimental study of flow past turbine blades

A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel

Tests of a small-scale NACA submerged inlet at transonic Mach numbers

An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2

Investigation of the NACA 4-(0)(03)-45 two-blade propeller at forward Mach numbers to 0.925

Investigation of a simple device for preventing separation due to shock and boundary-layer interaction

Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift

Investigation of an impulse axial-flow compressor rotor over a range of blade angles

Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing

Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections

Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method

Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35©�, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components

Performance of J33-A-27 Turbojet-Engine Compressor, II, Over - All Performance Characteristics of Modified Compressor at Equivalent Impeller Speeds from 6100 to 13,250 RPM

Static Longitudinal Stability of a Tandem-Coupled Bomber-Fighter Airplane Configuration Similar to One Proposed by Douglas Aircraft Company, Inc.

Static Longitudinal Stability of a Tandem-Coupled Bomber-Fighter Airplane Configuration Proposed by All American Airways, Inc.

Transonic Stability and Control Investigation of a 1/80-Scale Model of the Consolidated Vultee Skate 9 Seaplane, TED No. NACA DE 345: Transonic-Bump Method

Ditching Investigation of a 1/24-Scale Model of the Boeing B-47 Airplane

Preliminary Performance Data on Westinghouse Electronic Power Regulator Operating on J34-WE-32 Turbojet Engine in Altitude Wind Tunnel

Investigation of High-Subsonic Performance Characteristics of a 12 Degree 21-Inch Conical Diffuser, Including the Effects of Change in Inlet-Boundary-Layer Thickness

Tests of a Northrop XSSM-A-3 Missile in the Ames 40- by 80-Foot Wind Tunnel: Stability and Control

Calibration of Instruments for Measuring Wind Velocity and Direction

Investigation of Altitude Ignition, Acceleration, and Steady-State Operation with a Single Combustor of a J47 Turbojet Engine

Gust-Tunnel Investigation to Determine the Load at the Joint of a Coupled Airplane Configuration Encountering a Gust

General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions

Icing-protection requirements for reciprocating-engine induction systems

Flight experiences and tests on two airplanes with suction slots

Icing Characteristics and Anti-Icing Heat Requirements for Hollow and Ternally Modified Gas-Heated Inlet Guide Vanes

Analytical determination of local surface heat-transfer coefficients for cooled turbine blades from measured metal temperatures

Experimental and Analytical Study of Balanced-Diaphragm Fuel Distributors for Gas-Turbine Engines

Penetration of Air Jets Issuing from Circular, Square, and Elliptical Orifices Directed Perpendicularly to an Air Stream

Interpretation of boundary-layer pressure-rake data in flow with a detached shock

Fabrication and Properties of Hot-Pressed Molybdenum Disilicide

Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine

Investigation of first stage of two-stage turbine designed for free-vortex flow

Investigation of fretting corrosion by microscopic observation


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