Browse TRAIL Inventories

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

Effect of open circular holes on tensile strength and elongation of sheet specimens of a magnesium alloy

A survey of the aircraft-noise problem with special reference to its physical aspects

The theoretical characteristics of triangular-tip control surfaces at supersonic speeds: Mach lines behind trailing edges

Two-dimensional flow on general surfaces of revolution in turbomachines

Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter

Investigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing model

Critical study of integral methods in compressible laminar boundary layers

Buckling of rectangular sandwich plates subjected to edgewise compression with loaded edges simply supported and unloaded edges clamped

Calculation of aerodynamic forces on a propeller in pitch or yaw

Electrical techniques for compensation of thermal time lag of thermocouples and resistance thermometer elements

Effects of Aspect Ratio on Air Flow at High Subsonic Mach Numbers

An approximate method of determining the subsonic flow in an arbitrary stream filament of revolution cut by arbitrary turbomachine blades

Wing-body interference at supersonic speeds with an application to combinations with rectangular wings

Flame speeds of 2,2,4-trimethylpentane-oxygen-nitrogen mixtures

Torsion tests of aluminum-alloy stiffened circular cylinders


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