TRAIL - Technical Report Archive and Image Library

The interdependence of various types of autoignition and knock

Cooling Characteristics of the V-1650-7 Engine 2 - Effect of Coolant Conditions on Cylinder Temperatures and Heat Rejection at Several Engine Powers

Cooling Characteristics of the V-1650-7 Engine, 1, Coolant-Flow Distribution, Cylinder Temperatures, and Heat Rejections at Typical Operating Conditions

Preliminary Results of Altitude-Wind-Tunnel Investigation of X24C-4B Turbojet Engine. 5 - Performance of Modified Engine

Buffeting of External Fuel Tanks at High Speeds on a Grumman F7F-3 Airplane

Partial Measurements in Flight of the Flying Qualities of a Grumman XF7F-1 Airplane with a Modified Vertical Tail

Buffeting of External Fuel Tanks at High Speeds on a Gruman F7F-3 Airplane

Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8, and 19XB-1 Jet Propulsion Engines, 4 - Performance and Windmilling Drag Characteristics

Acceleration Characteristics of R-3350 Engine Equipped with NACA Injection Impeller

Determination of ram-jet combustion-chamber temperatures by means of total-pressure surveys

Determination of elastic stresses in gas-turbine disks

Effect of combustor-inlet conditions on performance of an annular turbojet combustor

Effect of fuel on performance of a single combustor of an I-16 turbojet engine at simulated altitude conditions

Design and performance of family of diffusing scrolls with mixed-flow impeller and vaneless diffuser

Analysis of performance of jet engine from characteristics of components I : aerodynamic and matching characteristics of turbine component determined with cold air

Analysis of effect of basic design variables on subsonic axial-flow-compressor performance

Effects of sweepback on boundary layer and separation

Altitude-Wind-Tunnel Investigation of R-4360-18 Power-Plant Installation for XR60 Airplane, 3, Performance of Induction and Exhaust Systems

Preliminary Results of Altitude-Wind-Tunnel Investigation of X24C-4B Turbojet Engine 1 - Pressure and Temperature Distributions

A simplified method of elastic-stability analysis for thin cylindrical shells

Knock-Limited Performance of Triptane and 28-R Fuel Blends as Affected by Changes in Compression Ratio and in Engine Operating Variables

Cooling of Gas Turbines, 3, Analysis of Rotor and Blade Temperatures in Liquid-Cooled Gas Turbines

A Preliminary Study of Ram-Actuated Cooling Systems for Supersonic Aircraft

Measurements in Flight of the Flying Qualities of a Chance Vought F4U-4 Airplane: TED No. NACA 2388

Minimum Specific Fuel Consumption of a Liquid-Cooled Multicylinder Aircraft Engine as Affected by Compression Ratio and Engine Operating Conditions

Performance of Compressor XJ-41-V Turbojet Engine 1 - Preliminary Investigation at Equivalent Compressor Speed of 8000 RPM

Performance Investigation of TG-180 Combustor: 1 - Instrumentation, Altitude Operational Limits and Combustion Efficiency

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel. V - Operational Characteristics, 5, Operational Characteristics

Isolated and cascade airfoils with prescribed velocity distribution

Hydrodynamic impact of a system with a single elastic mode I : theory and generalized solution with an application to an elastic airframe

Critical stress of thin-walled cylinders in axial compression

Wing plan forms for high-speed flight

Ditching Tests with a 1/12-Scale Model of the Army A-26 Airplane in Langley Tank No. 2 and on an Outdoor Catapult

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

Determination of Stress-Rupture Parameters for Four Heat-Resisting Alloys

Effects of temperature distribution and elastic properties of materials on gas-turbine-disk stresses

Preliminary Results of Altitude-Wind-Tunnel Investigation of X34C-4B Turbojet Engine. 3 - Compressor Performance, 3, Compressor Performance

Preliminary Results of Altitude-Wind-Tunnel Investigation of X24C-4B Turbojet Engine. 4 - Performance of Modified Compressor, Part 4, Performance of Modified Compressor

Investigation of pressure losses in several turbosupercharger nozzle hoses

Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a Mach number 1.5

Investigation of shock diffusers at Mach number 1.85 1: projecting single-shock cones

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

The Calculation of the Heat Required for Wing Thermal Ice Prevention in Specified Icing Conditions

Systematic Wind-Tunnel Measurements on a Laminar Wing With Nose Flap

Wind-Tunnel Investigation of Icing of an Engine Cooling-Fan Installation

A Flight Investigation of the Thermal Performance of Air Heated Propeller

Theoretical Investigation of Drag Reduction in Maintaining the Laminar Boundary Layer by Suction

Elastic Properties in Tension and Shear of High Strength Nonferrous Metals and Stainless Steel - Effect of Previous Deformation and Heat Treatment

Some Investigations of the General Instability of Stiffened Metal Cylinders 8: Stiffened Metal Cylinders Subjected to Pure Torsion

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