Investigation of slipstream effects on a wing-inlet oil-cooler ducting system of a twin-engine airplane in the Ames 40- by 80-foot wind tunnel

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

Computation of hinge-moment characteristics of horizontal tails from section data

The effect of wall interference upon the aerodynamic characteristics of an airfoil spanning a closed-throat circular wind tunnel

Measurements in flight of the pressure distribution on the right wing of a P-39N-1 airplane at several values of Mach number

Tunnel-wall corrections to rolling and yawing moments due to aileron deflection in closed rectangular wind tunnels

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

Wind-tunnel investigation of ailerons on a low-drag airfoil III : the effect of tabs

An Experimental Investigation of the Effect of Propellers Used as Aerodynamic Brakes on Stability and Control

Tests of an attack-type airplane in the Ames 40- by 80-foot wind tunnel to improve the high-speed maneuvering control-force characteristics

An investigation of the characteristics of alcohol-distribution tubes used for ice protection on aircraft windshields

An additional investigation of the high-speed lateral-control characteristics of spoilers

An investigation of 0.15-chord ailerons on a low-drag tapered wing at high speeds

A comparison of analytically and experimentally determined isothermal pressure losses in a heat-exchanger installation

An experimental investigation of the thrust and torque produced by propellers used as aerodynamic brakes

Measurements in flight of the stability, lateral control, and stalling characteristics of an airplane equipped with full-span Zap flaps and spoiler-type ailerons

Flight tests in several exhaust-gas-to-air heat exchangers in a b-17f airplane

Effect on the performance of a turbo-supercharged engine of an exhaust-gas-to-air heat exchange for thermal ice-prevention

Measurements in Flight of the Lateral-Control Characteristics of an Airplane Equipped with Full-Span Zap Flaps and Simple Circular-Arc-Type Ailerons

Preliminary investigation and design of an air-heated wing for Lockheed 12A airplane

A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane

A Flight Investigation of the Ice-Prevention Requirements of the United States Naval K-Type Airship

The effect of compressibility on two-dimensional tunnel-wall inerference for a symmetrical airfoil

A comparison of the effects of four-blade dual- and single-rotation propellers on the stability and control characteristics of a high-powered single-engine airplane

A flight investigation of the thermal properties of an exhaust heated wing de-icing system on a Lockheed 12-A airplane

An investigation of a thermal ice-prevention system for a C-46 cargo airplane VII : effect of the thermal system on the wing-structure stresses as established in flight

Flight tests of thermal ice-prevention equipment on a Lockheed 12A airplane

Effect of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls of a pursuit airplane equipped with a low-drag wing

Preliminary report on flight tests of an airplane having exhaust-heated wings

Wind-tunnel investigation of ailerons on a low-drag airfoil II : the effect of thickened and beveled trailing edges

Wind-tunnel investigation of ailerons on a low-drag airfoil I : the effect of aileron profile

Thermodynamic design of double-panel, air-heated windshields for ice prevention

Comparison of the energy method with the accelerometer method of computing drag coefficients from flight data

Observations of the improvement in vision brought about by the application of a rain-repellent lacquer on an airplane windshield

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

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

Flight investigation of the variation of drag coefficient with Mach number for the Bell P-39N-1 airplane

Correlation of the drag characteristics of a P-51B airplane obtained from high-speed wind-tunnel and flight tests

Investigation of Diving Moments of a Pursuit Airplane in the Ames 16-Foot High Speed Wind Tunnel

Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes

High-speed aerodynamic characteristics of a four-engine transport airplane as determined from tests of a 0.075-scale model

Flight measurements of the lateral control characteristics of an airplane equipped with a combination aileron-spoiler control system

High-speed wind-tunnel tests of a 1/14-scale model of a four-engine cargo airplane

Elimination of rumble from the cooling ducts of a single-engine pursuit airplane

Correlation of wind-tunnel predictions with flight tests of a twin-engine patrol airplane II : lateral- and directional-stability and control characteristics

The high-speed characteristics of several flaps and spoilers on the upper surface of the horizontal stabilizer of a model of a radial-engine pursuit airplane

The effect of amphibious floats on the power-off stability and control characteristics of a twin-engine cargo airplane

The effect of the skis on the power-off stability characteristics of a twin-engine cargo airplane

The effect of Mach number on the aerodynamic characteristics of a single-engine pursuit airplane as determined from tests of a 1/3-scale model

Investigation of the longitudinal stability at high speeds of a 1/5-scale model of a tailless pursuit airplane

Flying qualities of a high-speed bomber with a dual pusher propeller aft of the empennage as estimated from wind-tunnel tests of a 1/8-scale powered model

Flight measurements of the effect of various amounts of aileron droop on the low-speed lateral-control characteristics of an observation airplane

Kinetic temperature of wet surfaces : a method of calculating the amount of alcohol required to prevent ice, and the derivation of the psychometric equation

Wind Tunnel Investigation of the Effects of Slot Shape and Flap Location on the Characteristics of a Low-Drag Airfoil Equipped with a 0.25-Chord Slotted Flap

Flight measurements of horizontal tail loads on a typical propeller-driven pursuit airplane during stalled pull-outs at high speed

High-speed aerodynamic characteristics of a four-engine bomber airplane as determined from tests of a 0.075-scale model

High-speed wind-tunnel tests of semispan horizontal tails with fabric-covered and metal-covered elevators for a bomber airplane

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

Tests of the jet-motor air-intake duct system on a 1/4-scale stub-wing model of a pursuit-type airplane

Correlation of wind-tunnel predictions with flight tests of a twin-engine airplane I : longitudinal-stability and -control characteristics

Flight measurements of the effects of a wing leading-edge slot and other modifications on the stability, maximum lift, and high speed of an observation airplane

Aerodynamic characteristics of a 1/8-scale powered model of a high-speed bomber with a dual pusher propeller aft of the empennage

The Effects of a Highly Cambered Low-Drag Wing and of Auxiliary Flaps on the High-Speed Aerodynamic Characteristics of a Twin-Engine Pursuit Airplane Model

High-speed wind-tunnel tests of a 1/6-scale model of a twin-engine pursuit airplane

Wind-tunnel investigation of the effects of spoilers on the characteristics of a low-drag airfoil equipped with a 0.25-chord slotted flap

Flying qualities of a twin-engine patrol airplane as estimated from wind-tunnel tests

Wind-tunnel investigation of a 1/20-scale powered model of a four-engine transport airplane (Douglass and Dods, July 44)

Wind-tunnel investigation of a 1/20-scale powered model of the Douglas C-74 Airplane (Stevens, Douglass and Dods, May 44)

Fuel consumption corrected for cooling drag of an air-cooled radial aircraft engine at low fuel-air ratios and with variable spark advance