TRAIL - Technical Report Archive and Image Library

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

Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners : panels that fail by local buckling and have various values of width-to-thickness ratio for the webs of the stiffeners

Effect of yaw at supersonic speeds on theoretical aerodynamic coefficients of thin pointed wings with several types of trailing edge

Effect of reducing valve overlap on engine and compound-power-plant performance

Effect of Reynolds number in turbulent-flow range on flame speeds of Bunsen-burner flames

An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line designed to produce a high critical Mach number

Evaluation of a fixed spoiler as a gust alleviator

Effect of longitudinal stiffeners on the buckling load of long flat plates under shear

The effects of variations in Reynolds number between 3.0 x 10 to the power 6 and 25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

Effects of temporal tangential bearing acceleration on performance characteristics of slider and journal bearings

Effects of nacelle position on wing-nacelle interference

Estimation of effectiveness of flap-type controls on sweptback wings

Experimental investigation of the effects of plastic flow in a tension panel with a circular hole

The effect of fuel composition, compression pressure, and fuel-air ratio on the compression-ignition characteristics of several fuels

Tables of hypergeometric functions for use in compressible-flow theory

A statistical analysis of gust-velocity measurements as affected by pilots and airplanes

Supersonic wave drag of nonlifting sweptback tapered wings with Mach lines behind the line of maximum thickness

A simplified method for the determination and analysis of the neutral-lateral-oscillatory-stability boundary

Some fundamental similarities between boundary-layer flow at transonic and low speeds

Sound from dual-rotating and multiple single-rotating propellers

Sound-level measurements of a light airplane modified to reduce noise reaching the ground

Properties of 19-9DL alloy bar stock at 1200 F

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

Pressure-sensitive system for gas-temperature control

Cooling of gas turbines 9: cooling effects from use of ceramic coatings on water-cooled turbine blades

Analysis of variation of piston temperature with piston dimensions and undercrown cooling

The use of source-sink and doublet distributions extended to the solution of boundary-value problems in supersonic flow

Theoretical symmetric span loading at subsonic speeds for wings having arbitrary plan form

Altitude-Wind-Tunnel Investigation of Westinghouse 19B-2 19B-8, and 19XB-1 Jet-Propulsion Engines, Part 1, Operational Characteristics

Altitude-wind-tunnel investigation of tail-pipe burning with a Westinghouse X24C-4B axial-flow turbojet engine

Application of Theodorsen's theory to propeller design

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