TRAIL - Technical Report Archive and Image Library

Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness

Wing-flow tests of a triangular wing of aspect ratio two 1: effectiveness of several types of trailing-edge flaps on flat-plate models

Investigation of Rim Cracking in Turbine Wheels with Welded Blades

Stick-Fixed Stability and Control Characteristics of the Consolidated Vultee Model 240 Airplane as Estimated from Tests of a 0.092-Scale Powered Model

Flight Comparison of Performance and Cooling Characteristics of Exhaust-Ejector Installation with Exhaust-Collector-Ring Installation

Cooling of Gas Turbines, 2, Effectiveness of Rim Cooling of Blades

High-altitude flight cooling investigation of a radial air-cooled engine

Interference method for obtaining the potential flow past an arbitrary cascade of airfoils

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

Keyword Search

Published Year

Subject

Author