Browse TRAIL Inventories

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

Critical Stress of Ring-Stiffened Cylinders in Torsion

Vibration Survey of Blades in 10-Stage Axial-Flow Compressor 1: Static Investigation

Investigations on the Stability, Oscillation, and Stress Conditions of Airplanes With Tab Control: Second Partial Report: Application of the Solutions Obtained in the First Partial Report to Tab-Controlled Airplanes

Initial Experiments on Flutter of Unswept Cantilever Wings at Mach Number 1.3

High-Speed Wind-Tunnel Investigation of a Sweptback Wing With an Added Triangular Area at the Center

General Theory of Aerodynamic Instability and the Mechanism of Flutter

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)

Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)

Aerodynamic Properties of Cruciform-Wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds

A Statistical Study of Wave Conditions at Four Open-Sea Localities in the North Pacific Ocean

Ambient Pressure Determination at High Altitudes by Use of Free-Molecule Theory

Wind-tunnel investigation of the spinning characteristics of a model of a twin-tail low-wing personal-owner-type airplane with linked and unlinked rudder and aileron controls

The NACA oil-damped V-G recorder

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

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

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

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

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

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

First-order theory for unsteady motion of thin wings at supersonic speeds


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