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NACA Investigation of a Jet-Propulsion System Applicable to Flight

Wind Tunnel Investigation of Control Surface Characteristics: [Part] 12 - Various Cover-Plate Alinements on the NACA 0015 Airfoil With a 30 Percent Chord Flap and Large Sealed Internal Balance

Wind-tunnel investigation of profile drag and lift of an intermediate wing section of the XP-51 airplane with beveled trailing-edge and contour ailerons

Wind-tunnel investigation of control-surface characteristics 13: various flap overhangs used with a 30-percent-chord flap in an NACA 66-009 airfoil

Wind-Tunnel Investigation of the Characteristics of Blunt-Nose Ailerons on a Tapered Wing

Part-Throttle Operation and Control of a Piston-Ported Two-Stroke Cylinder

Representative Operating Charts of Propellers Tested in the NACA 20-Foot Propeller-Research Tunnel

Some Investigations of the General Instability of Stiffened Metal Cylinders 5: Stiffened Metal Cylinders Subjected to Pure Bending

A Hot-Wire Circuit With Very Small Time Lag

Principles of Moment Distribution Applied to Stability of Structures Composed of Bars or Plates

Thermodynamic Design of Double-Panel, Air-Heated Windshields for Ice Prevention

Emergency Measures for Increasing the Range of Fighter Airplanes

Analysis of Wind-Tunnel Stability and Control Tests in Terms of Flying Qualities in Full-Scale Airplanes

An Investigation of Aircraft Heaters 9: Measured and Predicted Performance of Two Exhaust Gas-Air Heat Exchangers and an Apparatus for Evaluating Exhaust Gas-Air Heat Exchangers

The effect of altitude on cooling

Derivation of charts for determining the horizontal tail load variation with any elevator motion

Adaptor for Measuring Principal Strains With Tuckerman Strain Gage

Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory

Performance of NACA eight-stage axial-flow compressor at simulated altitude

The NACA balanced-diaphragm dynamometer-torque indicator

Compressibility and Heating Effects on Pressure Loss and Cooling of a Baffled Cylinder Barrel

A Concise Theoretical Method for Profile-Drag Calculation; Advance Report

Profile-drag coefficients of conventional and low-drag airfoils as obtained in flight

Investigation of effects of various camouflage paints and painting procedures on the drag characteristics of an NACA 65 sub (421), sup -420, A = 1.0 airfoil section

Performance tests of wire strain gages 1: calibration factors in tension

Nondestructive test methods for spot welds in aluminum alloys

Effect of curvature on strength of axially loaded sheet-stringer panels

Bibliography of piston ring lubrication

Determination of stress-strain relations from "offset" yield strength values

Development of detonation detector suitable for use in flight

The shear of aluminum alloy driven rivets as affected by increasing D/t ratios

A unit laboratory engine oil system providing for a remote indication of oil flow and oil consumption together with blow-by measurement

An automatic electrical analyzer for 45 degree strain-rosette data

Numerical procedures for the calculation of the stresses in Monocoques I : diffusion of tensile stringer loads in reinforced panels

Numerical procedures for the calculation of the stresses in monocoques II : diffusion of tensiles stringer loads in reinforced flat panels with cut-outs

Charts for rapid analysis of 45 degree strain-rosette data

Elastic properties of channels with unflanged lightening holes

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

Wind-tunnel investigation of ailerons on a low-drag airfoil 1: The effect of aileron profile

Wind-tunnel investigation of the effects of profile modification and tabs on the characteristics of ailerons on a low-drag airfoil

Wind-tunnel investigation of ailerons on a low-drag airfoil 2: the effect of thickened and beveled trailing edges

Full-scale wind-tunnel investigation of forward underslung cooling-air ducts

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

High-altitude cooling VI : axial-flow fans and cooling power

High-altitude cooling IV : intercoolers

High-altitude cooling II : air-cooled engines

High-altitude cooling V : cowling and ducting

High-altitude cooling I : resume of the cooling problem

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

An investigation of aircraft heaters 17: experimental inquiry into steady state unidirectional heat-meter corrections


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