Browse TRAIL Inventories

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

Preliminary flight investigation of the wing-dropping tendency and lateral-control characteristics of a 35 degree swept-wing airplane at transonic Mach numbers

Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings

Effects of sweep on the damping-in-roll characteristics of three sweptback wings having an aspect ratio of 4 at transonic speeds

An NACA transonic test section with tapered slots tested at Mach numbers to 1.26

Performance of high-pressure-ratio axial-flow compressor using highly cambered NACA 65-series blower blades at high Mach numbers

NACA research on combustors for aircraft gas turbines I : effects of operating variables on steady-state performance

Large-scale flight measurements of zero-lift drag at Mach numbers form 0.86 to 1.5 of a wing-body combination having a 60 degree triangular wing with NACA 65A003 sections

Preliminary correlation of efficiency of aircraft gas-turbine combustors for different operating conditions

Preliminary analysis of effects of air cooling turbine blades on turbojet-engine performance

Preliminary investigation of constant-geometry, variable Mach number, supersonic tunnel with porous walls

Preliminary flight investigation of the dynamic longitudinal-stability characteristics of a 35 degree swept-wing airplane

Preliminary analysis of three cycles for nuclear propulsion of aircraft

Lift and moment characteristics at subsonic Mach numbers of four 10-percent-thick airfoil sections of varying trailing-edge thickness

Lateral-control investigation of flap-type and spoiler-type controls on a wing with quarter-chord-line sweepback of 60 degrees, aspect ratio 2, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bump method


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