TRAIL - Technical Report Archive and Image Library

Intercooler cooling-air weight flow and pressure drop for minimum drag loss

An investigation of aircraft heaters 15: the emissivity of several materials

An investigation of aircraft heaters 14: an air and heat flow analysis of a ram-operated heater and duct system

An investigation of aircraft heaters 24: the heat meter in the transient state for unidirectional heat transfer

An interim report on the stability and control of tailless airplanes

A method for welding sheet aluminum to SAE 4140 steel

A method for the rapid estimation of turbulent boundary-layer thickness for calculating profile drag

Loss of xylidines in overwater storage of xylidine-blended fuel

Performance tests of NACA type A finned-tube exhaust heat exchanger

Oxygen boosting of an aircraft-engine cylinder in conjunction with internal coolants

A preliminary evaluation of the explosion jet-propulsion engine

Longitudinal characteristics and aileron effectiveness of a midwing airplane from high-speed wind tunnel tests

Measurement of free water in cloud under conditions of icing

Flame-visibility tests with individual exhaust stacks

Flight tests of the thermal ice-prevention equipment on the B-17F airplane

Flight tests of various tail modifications on the Brewster XSBA-1 airplane III : measurements of flying qualities with tail configuration 3

Flight tests of several exhaust-gas-to-air heat exchangers

Flight tests of a pursuit airplane fitted with an experimental bellows-type bob weight

Gasoline-water distribution coefficients of 27 aromatic amines

Note on the interpretation of wake-survey data and its use in the estimation of induced drag due to irregularities

Wind-Tunnel Procedure for Determination of Critical Stability and Control Characteristics of Airplanes

The effect of compression ratio, cooled exhaust gas mixed with inlet air, and inlet-air temperature on the knock-limited performance of a full-scale single-cylinder engine

The effect of continuous knock on the endurance of an aircraft engine cylinder

Effect of coaxial lapping of cast-iron piston rings on ring performance

Knock-limited performance of several internal coolants

Ditching tests with a 1/12-size model of the Army B-26 airplane in NACA tank number 2 and on an outdoor catapult

Determination of jet-boundary corrections to cowling-flap-outlet pressures by an electrical analogy method

The design of the optimum hull for a large long-range flying boat

Preignition-limited performance of several fuels

Knock-limited power outputs from a CFR engine using internal coolants 1: monomethylamine and dimethylamine

Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing

Airfoil section data from tests of 10 practical- construction sections of helicopter rotor blades submitted by the Sikorsky Aircraft Division, United Aircraft Corporation

Airfoil-contour modifications based on (epsilon)-curve method of calculating pressure distribution

Cascade investigation of buckets for a modern aircraft turbosupercharger

An analytical investigation of thermal-electric means of preventing ice formations on a propeller blade

Bending and shear stresses developed by the instantaneous arrest of the root of a moving cantilever beam

Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel

Compressible potential flow with circulation about a circular cylinder

Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes

Analysis of a thermal ice-prevention system for wing leading-edge landing-light installations

Analysis of available data on the effectiveness of ailerons without exposed overhang balance

Effect of water injection on knock-limited performance of a V-type 12-cylinder liquid-cooled engine

Effect of tilt of the propeller axis on the longitudinal-stability characteristics of single-engine airplanes

Determination of the effect of wing flexibility on lateral maneuverability and a comparison of calculated rolling effectiveness with flight results

The determination of span load distribution at high speeds by use of high-speed wind-tunnel section data

Effect of tilt of the propeller axis on the longitudinal-stability characteristics of single-engine airplanes

Estimation of pressures on cockpit canopies, gun turrets, blisters, and similar protuberances

Estimation of pressure distributions at subcritical speeds for turrets located on a wing

Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails

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