Browse TRAIL Inventories

Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement

Comparison of theoretical and experimental heat transfer on a cooled 20 degrees cone with a laminar boundary layer at a Mach number of 2.02

A comparison of theoretical and experimental wing bending moments during seaplane landings

Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane model

Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow

The development and performance of two small tunnels capable of intermittent operation at Mach numbers between 0.4 and 4.0

Investigation of spark-over voltage - density relation for gas-temperature sensing

Application of the wire-mesh plotting device to incompressible cascade flows

Relation Between Inflammables and Ignition Sources in Aircraft Environments

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

Stress and distortion measurements in a 45 degree swept box beam subjected to antisymmetrical bending and torsion

Stress and strain concentration at a circular hole in an infinite plate

Spectrums and diffusion in a round turbulent jet

Spin-tunnel investigation to determine the effect on spin recoveries of reducing the opening shock load of spin-recovery parachutes

The calculation of downwash behind wings of arbitrary plan form at supersonic speeds

The calculation of modes and frequencies of a modified structure from those of the unmodified structure

Theoretical analysis of various thrust-augmentation cycles for turbojet engines

Density fields around a sphere at Mach numbers 1.30 and 1.62

Maximum pitching angular accelerations of airplanes measured in flight

Gust-tunnel investigation of a wing model with semichord line swept back 60 degrees

Charts of thermodynamic properties of air and combustion products from 300 degrees to 3500 degrees R

The dynamic lateral control characteristics of airplane models having unswept wings with round-and sharp-leading-edge sections

Graphical method for obtaining flow field in two-dimensional supersonic stream to which heat is added

The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A- series airfoil section

Properties of a boron carbide-iron ceramal

Sintering mechanism between zirconium carbide and columbium

Laminar-boundary-layer heat-transfer characteristics of a body with a pressure gradient at supersonic speeds

General method for computation of equilibrium composition and temperature of chemical reactions

Tables of thermodynamic functions for analysis of aircraft-propulsion systems

Boundary-layer measurements in 3.84- by 10-inch supersonic channel

Theoretical turbojet thrust augmentation by evaporation of water during compression as determined by use of a Mollier diagram

Method for determining optimum division of power between jet and propeller for maximum thrust power of a turbine-propeller engine

A survey of the flow at the plane of the propeller of a twin-engine airplane

Investigation of flap-type ailerons on an untapered wing having an aspect ratio of 3.7, 45 degree sweepback, and an NACA 65A009 airfoil section : transonic-bump method

Flight determination of the effects of rudder-pedal-force characteristics on the aiming error in azimuth of a conventional fighter airplane

Initial flight investigation of a twin engine supersonic ram jet

Fundamental flame velocities of pure hydrocarbons 2: alkadienes

Fundamental flame velocities of pure hydrocarbons 1: alkanes, alkenes, alkynes benzene, and cyclohexane

High-speed aerodynamic characteristics of a lateral-control model 3: section characteristics, fence studies, and tabulated pressure coefficients with modified NACA 0012-64 section, 26.6-percent-chord, plain aileron, 0 and 45 degree sweepback

Investigation of perforated convergent-divergent diffusers with initial boundary layer

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback: Static longitudinal stability and control characteristics at a Mach number of 1.59

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.59

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : static lateral stability characteristics at Mach numbers of 1.40 and 1.59

Investigation of a 1/5-scale model of a proposed high-submerged-speed submarine in the Langley full-scale tunnel

Investigation of ignition characteristics of AN-F-32 and two AN-F-58a fuels in single can-type turbojet combustor

The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests

Tests of a small-scale NACA submerged inlet at transonic Mach numbers

Influence of tube-entrance configuration on average heat-transfer coefficients and friction factors for air flowing in an Inconel tube

Investigation of stage performance of X24C-2 ten-stage axial-flow compressor at design speed


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