TRAIL - Technical Report Archive and Image Library

Flight measurements of the lateral control characteristics of narrow-chord ailerons on the trailing edge of a full-span slotted flap

Field of Flow About a Jet and Effect of Jets on Stability of Jet-Propelled Airplanes

Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Model with Wing Flaps Deflected 15 Degrees, TED No. NACA 2387

Internal and external aerodynamics of ducted bodies at supersonic speeds

Investigation of the Pressure-Loss Characteristics of the Westinghouse X24-C-2 Inlet Screen, TED No. NACA 0447

Standard nomenclature for airspeeds with tables and charts for use in calculation of airspeed

Waters Loads on the XJL-1 Hull as Obtained in Langley Impact Basin, TED No. NACA 2413.3

Parameters determining performance of supersonic pilotless airplanes powered by ram-compression power planes

Paths of target-seeking missiles in two dimensions

Wind-Tunnel Tests of a Modified Koppers Aeromatic Impeller-Generator Combination, TED No. NACA ARR 2901

A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds

Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient

Flight tests of experimental beveled-trailing-edge Frise ailerons on a fighter airplane

Flutter and oscillating air-force calculations for an airfoil in two-dimensional supersonic flow

Flow over a slender body of revolution at supersonic velocities

Theoretical lift and drag of thin triangular wings at supersonic speeds

Tank tests to determine the effect on planing-tail hulls of varying length, width, and plan-form taper of afterbody

Summary of lateral-control research

Two dimensional wind-tunnel investigation of low drag vertical-tail,horizontal-tail, and wing sections equipped with sealed internally balanced control surfaces

Wind-tunnel investigation of end-plate effects of horizontal tails on a vertical tail compared with available theory

The Lagrangian Multiplier Method of Finding Upper and Lower Limits to Critical Stresses of Clamped Plates

Analysis of Available Data on the Effects of Tabs on Control-Surface Hinge Moments

Analysis of Deep Rectangular Shear Web Above Buckling Load

Effect of Distance on Airplane Noise

Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane

An experimental investigation of NACA submerged air inlets on a 1/5-scale model of a fighter airplane

Influence of wall boundary layer upon the performance of an axial-flow fan rotor

The effect of high solidity on propeller characteristics at high forward speeds from wind-tunnel tests of the NACA 4-(3)(06.3)-06 and NACA 4-(3)(06.4)-09 two-blade propellers

Performance of compressor blade cascades at high Mach numbers

The NACA mixture analyzer and its application to mixture-distribution measurement in flight

Some Recent Contributions to the Study of Transition and Turbulent Boundary Layers

An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought XF7U-1 Airplane in the Langley High-Speed 7- by 10-Foot Tunnel. Part IV - Aileron Characteristics TED No. NACA DE308, Part 4, Aileron Characteristics, TED No. NACA DE308

High-Speed Load Distribution of the Wing of a 3/16-Scale Model of the Douglas XSB2D-1 Airplane with Flaps Deflected

Effect of Exhaust Pressure on the Cooling Characteristics of a Liquid-Cooled Engine

Wind-Tunnel Investigation of the Low-Speed Characteristics of a 1/8-Scale Model of the Republic XP-91 Airplane with a Vee and a Conventional Tail

The Effectiveness at High Speeds of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil

Stability and Control Characteristics of a 1/10-Scale Model of the McDonnell XP-85 Airplane While Attached to the Trapeze

Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Static Longitudinal Stability of Models with Wing Flap Deflections of 0 Deg and 15 Deg, TED No. NACA 2387

Recent Results on High-Pressure Axial Blowers

Investigations of Compression Shocks and Boundary Layers in Gases Moving at High Speed

Pressure Distribution Measurements at High Speed and Oblique Incidence of Flow

Lift and Drag of Wings with Small Span

Possibilities of Reducing the Length of Axial Superchargers for Aircraft Motors

Cooling of Gas Turbines, IV - Calculated Temperature Distribution in the Trailing Part of a Turbine Blade Using Direct Liquid Cooling

Effects of Compressibility on the Flow Past Thick Airfoil Sections

An Anaylsis of Control Requirements and Control Parameters for Direct-Coupled Turbojet Engines

Preliminary Evaluation of the Low-Speed Stability and Control Characteristics of the McDonnell XP-85 Airplane from Tests of an Unballasted 1/5-Scale Model in the Langley Free-Flight Tunnel

Preliminary Evaluation of the Spin and Recovery Characteristics of the Douglas XF3D-1 Airplane

High-Speed Load Distribution on the Wing of a 3/16-Scale Model of a Scout-Bomber Airplane with Flaps Deflected

A Comparison of Three Theoretical Methods of Calculating Span Load Distribution on Swept Wings

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