TRAIL - Technical Report Archive and Image Library

Investigation of the Aerodynamic Effects of an External Store in Combination With 60 Degree Delta and Low-Aspect-Ratio Tapered Wings at a Mach Number of 1.9

An Investigation of Four Wings of Square Plan Form at a Mach Number of 6.86 in the Langley 11-Inch Hypersonic Tunnel

An Investigation of the Longitudinal Characteristics of the X-3 Configuration With Wing and Horizontal Tail Surfaces of Aspect Ratio 3.0 by Means of Rocket-Propelled Models: Results at High Lift Coefficients

Free-Spinning Tunnel Investigation of a 1/20-Scale Model of the Douglas X-3 Airplane

Flight Performance of a Twin-Engine Supersonic Ram Jet From 2,300 to 67,200 Feet Altitude

Free-Flight Investigation to Determine Force and Hinge-Moment Characteristics at Zero Angle of Attack of a 60 Degrees Sweptback Half-Delta Tip Control on a 60 Degrees Sweptback Delta Wing at Mach Numbers Between 0.68 and 1.44

Free-Jet Tests of a 6.5-Inch-Diameter Ram-Jet Engine at Mach Numbers 1.81 and 2.00

An Investigation at Transonic Speeds of the Effects of Control Chord and Span on the Control Characteristics of a Tapered Wedge-Type Wing of Aspect Ratio 2.5: Transonic-Bump Method

Investigation at Mach Number 1.88 of Half of a Conical-Spike Diffuser Mounted as a Side Inlet With Boundary-Layer Control

Wind-Tunnel Investigation at Low Speed of the Effects of Symmetrical Deflection of Half-Delta Tip Controls on the Damping in Roll and Yawing Moment Due to Rolling of a Triangular-Wing Model

A Comparison of Theory and Experiment for High-Speed Free-Molecule Flow

The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow

Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow

An analysis of an x-ray absorption method for measurement of high gas temperatures

Development of Auxiliary Cyclotron Equipment for Using Tritium as Bombarding Particles in a Cyclotron

Contributions to the theory of the spreading of a free jet issuing from a nozzle

Approximate method of integration of laminar boundary layer in incompressible fluid

Gas flow with straight transition line

Experiments on transonic flow around wedges

Sound from a two-blade propeller at supersonic tip speeds

Mechanism of start and development of aircraft crash fires

Electrical Pressure Integrator

Abnormal Grain Growth in S-816 Alloy

Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications

Error in airspeed measurement due to static-pressure field ahead of an open-nose air-inlet model at transonic speeds

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients

Flutter of a 60©� delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model

Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds

Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61

A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36©�

Heat transfer and skin friction for turbulent boundary layers on heated or cooled surfaces at high speeds

Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel

Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel

Low-Speed Wind-Tunnel Investigation of the Drag of a Lockheed F-94C Airplane (A.F. No. 50-956)

Free-Flight-Tunnel Investigation of the Dynamic Stability and Control Characteristics of a Chance Vought F7U-3 Airplane in Towed Flight

As Investigation at Mach Numbers of 1.41 and 2.01 of the Aerodynamic Characteristics of an 0.025-scale Model of the MX-1712

An Investigation of the Effect of the WADC 30,000-Horsepower Whirl Rig Upon the Static Characteristics of a Propeller

Effect of Various Blade Modifications in Performance of a 16-Stage Axial-flow Compressor. IV - Effect on Over-all Performance Characteristics of Decreasing Twelfth through Fifteenth Stage Stator-blade Angles 3 deg and Increasing Stator Angles in the Inlet Stages

A Photographic Study of Freezing of Water Droplets Falling Freely in Air

Preliminary Survey of Icing Conditions Measured During Routine Transcontinental Airline Operation

Impingement of Water Droplets on an NACA 65(sub 1) -212 Airfoil at an Angle of Attack of 4 Deg

The Calculated and Measured Performance Characteristics of a Heated-Wire Liquid-Water-Content Meter for Measuring Icing Severity

Experimental Investigation of Average Heat-Transfer and Friction Coefficients for Air Flowing in Circular Tubes Having Square-Thread-Type Roughness

Experimental and theoretical determination of thermal stresses in a flat plate

Flow characteristics over a lifting wedge of finite aspect ratio with attached and detached shock waves at a Mach number of 1.40

Investigation of hydrocarbon ignition

A blade-element analysis for lifting rotors that is applicable for large inflow and blade angles and any reasonable blade geometry

Landing characteristics in waves of three dynamic models of flying boats

Effect of compressibility on the flow past a two-dimensional bump

Effect of changing passage configuration on internal-flow characteristics of a 48-inch centrifugal compressor

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