TRAIL - Technical Report Archive and Image Library

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

An investigation of the effect of tip shape on the low-speed aerodynamic characteristics of large-scale swept wings

Analytical comparison of a standard turbojet engine, a turbojet engine with a tail-pipe burner, and a ram-jet engine

Investigation of carbon deposition in an I-16 jet-propulsion engine at static sea-level conditions

Cooling of gas-turbines 7: effectiveness of air cooling of hollow turbine blades with inserts

Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine II: performance with water injection at compressor inlet

Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine 3: performance with tail-pipe burning in standard-size tail pipe

Application of an ultraviolet spectrophotometric method to the estimation of alkylnaphthalenes in 10 experimental jet-propulsion fuels

Experimental investigation of performance and operating characteristics of a tail-pipe burner for a turbojet engine

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

Investigation of wing characteristics at a Mach number of 1.53 1: triangular wings of aspect ratio 2

The calculation of drag for airfoil sections and bodies of revolution at subcritical speeds

Investigation of shock diffusers at Mach number 1.85 2: projecting double-shock cones

Investigation of shock diffusers at Mach number 1.85 3: multiple-shock and curved-contour projecting cones

An approximate method for calculating the effect of surface roughness on the drag of an airplane

An Investigation of Convergent-Divergent Diffusers at Mach Number 1.85

A comparison with flight data of vertical-tail loads in various maneuvers estimated from sideslip angles and rudder deflections

Experimental investigation of thrust augmentation of a turbojet engine at zero ram by means of tail-pipe burning

Test-stand investigation of a rectangular ram-jet engine

A summary and analysis of data on dive-recovery flaps

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

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

Experimental investigation of velocity distributions of downstream of single duct bends

Subsonic flow over thin oblique airfoils at zero lift

Performance of a double-row radial aircraft engine with three methods of safety-fuel injection

High-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wing

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