TRAIL - Technical Report Archive and Image Library

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

Aerodynamic measurements made during Navy investigation of human tolerance to wind blasts

Theoretical investigation of thrust augmentation of turbojet engines by tail-pipe burning

Performance of a 20-inch steady-flow ram jet at high altitudes and ram-pressure ratios

High-speed wind-tunnel investigation of the effects of compressibility on a pitot-static tube

An empirically derived method for calculating pressure distribution at supercritical Mach numbers and moderate angles of attack

Knock-limited power outputs from a CFR engine using internal coolants III : four alkyl amines, three alkanolamines six amides, and eight heterocyclic compounds

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

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