Browse TRAIL Inventories

Comparison between flight-measured and calculated span load distribution at high Mach numbers

The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions

Investigation of Thrust Augmentation of a 1600-Pound Thrust Centrifugal-Flow-Type Turbojet Engine by Injection of Refrigerants at Compressor Inlets

Measurements of the damping in roll of large-scale swept-forward and swept-back wings

Fuel investigation in a tubular-type combustor of a turbojet engine

Preliminary investigation of effects of alpha-particle bombardment on the creep rate of aluminum

A suggested method of analyzing for transonic flutter of control surfaces based on available experimental evidence

Fuel tests on an I-16 jet-propulsion engine at static sea-level conditions

A fuel-distribution control for continuous-flow manifold injection on reciprocating engines

The use of perforated inlets for efficient supersonic diffusion

An analysis of longitudinal-control problems encountered in flight at transonic speeds with a jet-propelled airplane

Characteristics of a 15-percent-chord and a 35-percent-chord plain flap on the NACA 0006 airfoil section at high subsonic speeds

Combustion-efficiency investigation of special fuels in single tubular-type combustor at simulated altitude conditions

Computed performance of a composite engine based on experimental data for a single-cylinder conventional aircraft engine converted to compression-ignition operation

Flight investigation of the heat requirements for ice prevention on aircraft windshields

A summary report on the effects of Mach number on the span load distribution on wings of several models

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


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