TRAIL - Technical Report Archive and Image Library

Calculated and measured turning performance of a Navy F2A-3 airplane as affected by the use of flaps

Laminar-boundary-layer oscillations and transition on a flat plate

De-icing of an aircraft-engine induction system

Bearing strengths of bare and alclad XA75S-T and 24S-T81 aluminum alloy sheet

Methods of Measurement of High Air Velocities by the Hot-Wire Method

The effect of inlet-valve design, size, and lift on the air capacity and output of a four-stroke engine

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

The flow of a compressible fluid past a curved surface

NACA Mach number indicator for use in high-speed tunnels

The Measurement of Fuel-Air Ratio by Analysis for the Oxidized Exhaust Gas

Flight tests of thermal ice-prevention equipment in the XB-24F airplane

Icing tests of aircraft-engine induction systems

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

Ditching tests with 1/10-size model of the Army A-20A airplane I : calm-water tests in NACA tank no.2

Determination of general relations for the behavior of turbulent boundary layers

The problem of longitudinal stability and control at high speeds

Laminar-boundary-layer oscillations and transition on a flat plate

Some Investigations of the General Instability of Stiffened Metal Cylinders 7: Stiffened Metal Cylinders Subjected to Combined Bending and Torsion

Tests of Aluminum-Alloy Stiffened-Sheet Specimens Cut From an Airplane Wing

Torsional Elastic Properties of 18:8 Chromium-Nickel Steel as Affected by Plastic Deformation and by Heat Treatment

Turbulent Flow Between Rotating Cylinders

Large-Deflection Theory of Curved Sheet

Large-Deflection Theory for End Compression of Long Rectangular Plates Rigidly Clamped Along Two Edges

Effect of Rivet Pitch Upon the Fatigue Strength of Single-Row Riveted Joints of 0.025- to 0.025-Inch 24S-T Alclad

Effects of Prior Fatigue-Stressing of the Impact Resistance of Chromium-Molybdenum Aircraft Steel

Description of Stress-Strain Curves by Three Parameters

The Stability of Isotropic or Orthotopic Cylinders or Flat or Curved Panels, Between and Across Stiffeners, With Any Edge Conditions Between Hinged and Fixed, Under Any Combination of Compression and Shear

The Strength of Thin-Wall Cylinders of D Cross Section in Combined Pure Bending and Torsion

Round Heat-Treated Chromium-Molybdenum-Steel Tubing Under Combined Loads

Tensile and Compressive Tests of Magnesium Alloy J-1 Sheet

A Theoretical Investigation of the Rolling Oscillations of an Airplane With Ailerons Free

A Theoretical Investigation of the Lateral Oscillations of an Airplane With Free Rudder With Special Reference to the Effect of Friction

Progress Report on Fatigue of Spot-Welded Aluminum

Protection of Nonmetallic Aircraft From Lighting 1: General Analysis

Protection of Nonmetallic Aircraft From Lightning 2: Lightning Conductor Materials

The Flow of a Compressible Fluid Past a Curved Surface

Working Charts for the Computation of Propeller Thrust Throughout the Take-Off Range

Tests of a 1/40-Scale Wing-Hull Model and a 1/10-Scale Float-Strut Model of the Hughes-Kaiser Cargo Airplane in the Two-Dimensional Low-Turbulence Pressure Tunnel

Tests of Airfoils Designed to Delay the Compressibility Burble

Tests in the NACA Two-Dimensional Low-Turbulence Tunnel of Airfoil Sections Designed to Have Small Pitching Moments and High Lift-Drag Ratios

Porpoising: A Comparison of Theory With Experiment

Wind-Tunnel Investigation of Wing Ducts on a Single Engine Pursuit Airplane

Methods and Charts for Computing Stability Derivatives of a V-Bottom Planing Surface

Effect of Length-Beam Ration on Resistance and Spray of Three Models of Flying-Boat Hulls

Investigation for the Development of a High-Speed Antiaircraft Tow Target

Free-Flight-Tunnel Investigation of the Effect of Mode of Propeller Rotation Upon the Lateral-Stability Characteristics of a Twin-Engine Airplane Model With Single Vertical Tails of Different Size

Flying Qualities and Stalling Characteristics of North American XP-51 Airplane

Experimental Determination of the Yawing Moment Due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model

Construction of Wire Strain Gages for Engine Application

Preliminary Aerodynamic and Structural Tests Showing the Effect of Compressive Load on the Fairness of a Low-Drag Wing Specimen With Chordwise Hat-Section Stiffeners

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