Browse TRAIL Inventories

Characteristics of a Sealed Internally Balanced Aileron from Tests of a 1/4-Scale Partial-Span Model of the Republic XF-12 Airplane in the Langley 19-Foot Pressure Tunnel

Effects of Wing Flaps and Wing Duct Inlet on the Lift and Stalling Characteristics of a 1/4-Scale Partial-Span Model of the Republic XF-12 Airplane in the Langley 19-Foot Pressure Tunnel

Evaluation of Gust and Draft Velocities from Flights of P-61c Airplanes within Thunderstorms. 3 - July 12, 1946 to July 18, 1946 at Orlando, Florida

Development of Wing Inlets

Effect of an Auxiliary Belly Fuel Tank on the Low-Speed Static Stability Characteristics of a 1/5-Scale Model of the Grumman XF8F-1 Airplane, TED No. NACA 2384

Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil Sections

Method for calculating wing characteristics by lifting-line theory using nonlinear section lift data

Tank Tests of a 1/7-Size Powered Dynamic Model of the Grumman XJR2F-1 Amphibian: Spray Characteristics, Take-Off and Landing Stability in Smooth Water - Langley Tank Model 212, TED No. NACA 2378

Tank Tests of an Alternate Hull Form for the Consolidated Vultee PB2Y-3 Airplane

Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms: August 23, 1946 to September 4, 1946 at Orlando, Florida

Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms. 4 - July 19, 1946 to July 20, 1946 at Orlando, Florida

Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms August 21, 1946 to August 22, 1946 at Orlando, Florida

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

Force Tests of the Boeing XB-47 Full-Scale Empennage in the Ames 40- by 80-Foot Wind Tunnel

Performance of Compressor of XJ-41-V Turbojet Engine, 3, Compressor Static-Pressure Rise at Equivalent Compressor Speeds of 5000, 7000, 8000, and 9000 rpm

Altitude Cooling Investigation of the R-2800-21 Engine in the P-47G Airplane. IV - Engine Cooling-Air Pressure Distribution

Preliminary Investigation of Over-all Performance of Experimental Turbojet Engine for Guided Missiles

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

Tests of the Landing on Water of a Model of a High-Speed Airplane - Langley Tank Model 229

Icing Properties of Noncyclonic Winter Stratus Clouds

Investigation of suction-slot shapes for controlling a turbulent boundary layer

A method for numerically calculating the area and distribution of water impingement on the leading edge of an airfoil in a cloud

Effects of sweepback on boundary layer and separation

A method for calculating the heat required for windshield thermal ice prevention based on extensive flight tests in natural icing conditions

Investigation of effects of surface temperature and single roughness elements on boundary-layer transition

Flight tests of a double-hinged horizontal tail surface with reference to longitudinal-stability and control characteristics


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