Browse TRAIL Inventories

Preliminary investigation of hydrazine as a rocket fuel

A comparison of the simulated-altitude performance of two turbojet combustor types

Control during starting of gas-turbine engines

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

A flight investigation and analysis of the lateral-oscillation characteristics of an airplane

Theoretical analysis of the performance of a supersonic ducted rocket

An investigation of the downwash and wake behind large-scale swept and unswept wings

Vibration of turbine blades in a turbojet engine during operation

Investigation of the diborane - hydrogen peroxide propellant combination

Effect of three flame-holder configurations on subsonic flight performance of rectangular ram jet over range of altitudes

Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by injection of water and alcohol at compressor inlets

Experimental investigation of thrust augmentation of axial-flow-type 4000-pound-thrust turbojet engine by water and alcohol injection at compressor inlet

Investigation of two pitot-static tubes at supersonic speeds

Additional free-flight tests of the rolling effectiveness of several wing-spoiler arrangements at high subsonic, transonic, and supersonic speeds

Ditching Tests of a 1/8-Scale Model of the Chance Vought XF6U-1 Airplane, TED No. NACA DE319

Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine, 7, Pressure and Temperature Distributions

Performance of conical jet nozzles in terms of flow and velocity coefficients

Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, Part 1, Performance and Windmilling Drag Characteristics

Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine. 2 - Operational Characteristics

Full-scale investigation of aerodynamic characteristics of a typical single-rotor helicopter in forward flight

Effect of centrifugal force on the elastic curve of a vibrating cantilever beam

Measurements in Flight of the Longitudinal-Stability Characteristics of a Republic YF-84A Airplane (Army Serial No. 45-59488) at High Subsonic Mach Numbers

Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine 1 - Analysis of Turbine Performance

Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine 2 - Analysis of Compressor Performance

Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, 4 - Analysis of Compressor Performance

Correlation of the drag characteristics of a typical pursuit airplane obtained from high-speed wind-tunnel and flight tests

An analytical method of estimating turbine performance

Analysis of Effects of Inlet Pressure Losses on Performance of Axial-Flow Type Turbojet Engine

Hydrodynamic Characteristics of an Aerodynamically Refined Planing-Tail Hull

Determination of stresses in gas-turbine disks subjected to plastic flow and creep

Estimation of F-3 and F-4 knock-limited performance ratings for ternary and quaternary blends containing triptane or other high-antiknock aviation-fuel blending agents

An experimental investigation of the design variables for NACA submerged duct entrances

Performance of Allison Model 400-C6 Turbojet-Engine Compressor, 1: Over-All Performance Characteristics of Compressor at Equivalent Impeller Speeds of 6000, 7000, and 8500 RPM

Calibration of Air-Flow Meters for J33 Compressor Investigation

An Investigation of the McDonnell XP-85 Airplane in the Ames 40- by 80-Foot Wind Tunnel: Pressure-Distribution Tests

An Investigation of the McDonnell XP-85 Airplane in the Ames 40- by 80-foot Wind Tunnel. Force and Moment Tests

Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine, 4, Operational Characteristics

Design Data for Graphical Construction of Two-Dimensional Sharp-Edge-Throat Supersonic Nozzles

Performance Investigations of a Large Centrifugal Compressor from an Experimental Turbojet Engine

Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, 3, Performance Characteristics with the High-Flow Compressor

Simulated Altitude Performance of Combustors for the 24C Turbojet Engine. III - Performance of Rectangular-Slot Baskets, 3, Performance of Rectangular-Slot Baskets

High-Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 0.10-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE301

A general small-deflection theory for flat sandwich plates

Subsonic flow over thin oblique airfoils at zero lift

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine VI : combustion-chamber performance

Altitude-wind-tunnel investigation of operational characteristics of Westinghouse X24C-4B axial flow turbojet engine

Linear theory of boundary effects in open wind tunnels with finite jet lengths

Equations for the design of two-dimensional supersonic nozzles

Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers

Knocking combustion observed in a spark-ignition engine with simultaneous direct and Schlieren high-speed motion pictures and pressure records


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