TRAIL - Technical Report Archive and Image Library

Experimental evaluation by thermodynamic methods of work input to a centrifugal compressor operating with water injection

Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration-Cooled Walls with Application to Turbine Blade Cooling

Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 III : conical-spike all-external-compression inlet with supersonic cowl lip

Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 1: conical spike all-external compression inlet with subsonic cowl lip

Fatigue strengths of aircraft materials: axial-load fatigue tests on notched sheet specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with stress-concentration factors of 2.0 and 4.0

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness at supersonic speeds of a 30-percent chord, 50-percent semispan elevon as a lateral control device

Preliminary investigation of the delay of turbulent flow separation by means of wedge-shaped bodies

Preliminary investigation of the supersonic flow field downstream of wire-mesh nozzles in a constant-area duct / Lawrence I. Gould

Some effects of solidity on turning through constant-thickness circular-arc guide vanes in axial annular flow

Studies of high-temperature protection of a titanium-carbide ceramal by chromium-type ceramic-metal coatings

Review of some recent data on buffet boundaries

Transonic flow past a wedge profile with detached bow wave : details of analysis

Wing-flow investigation of the characteristics of seven unswept, untapered airfoils of aspect ratio 8.0

Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a high-aspect-ratio bomber model with self-supporting free-floating fuel tanks attached to the wing tips

Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a tip-to-tip bomber-fighter coupled airplane configuration

Investigation of annular liquid flow with concurrent air flow in horizontal tubes

An investigation of the spray characteristics of a jet-powered dynamic model of the drag flying boat with a vee tail : TED No. NACA DE 328

Free-flight performance of 16-inch diameter supersonic ram-jet units 4: performance of ram-jet units designed for combustion chamber inlet Mach number of 0.21 at free-stream Mach number of 1.6 over a range flight conditions

A comparison of the experimental and theoretical loading over triangular wings in sideslip at supersonic speeds

A comparison of the calculated maximum-maneuver response characteristics of three air-to-air, beam-rider, guided missiles having different lift ratios

A comparison of the experimental and theoretical loading over triangular wings at supersonic speeds

Effect of blade-surface finish on performance of a single-stage axial-flow compressor

Design and performance of an experimental axial-discharge mixed-flow compressor II : over-all performance of impeller and supersonic-diffuser combination

Damping in a roll of a missile configuration with a modified triangular wing and a cruciform tail at a Mach number of 1.52

Effects of spanwise thickness variation on the transonic aerodynamic characteristics of wings having 35 degrees of sweepback, aspect ratio 4, and taper ratio 0.60

Effects of spanwise thickness variation on the aerodynamic characteristics of 35 degree and 45 degree sweptback wings of aspect ratio 6: transonic-bump method

Application of Theodorsen's propeller theory to the calculation of the performance of dual-rotating propellers

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution, cambered and twisted for a trapezoidal span load distribution

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: twisted and cambered triangular wing of aspect ratio 2 with NACA 0003-63 thickness distribution

A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers

Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder

An investigation of convergent-divergent diffusers at Mach number 1.85

Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration

A velocity-correction formula for the calculation of transonic Mach number distributions over diamond-shaped airfoils

Velocity and temperature fields in circular jet expanding from choked nozzle into quiescent air

Laminar friction and heat transfer at Mach numbers from 1 to 10

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution, cambered and twisted for trapezoidal span load distribution

On the angular distribution of slip lines in polycrystalline aluminum alloy

Compilation and review of effects of design parameters on ditching characteristics

Investigation at low speed of the effectiveness and hinge moments of a constant-chord elevator on a large-scale triangular wing with section modification

An investigation at Mach numbers of 1.40 and 1.59 of the effects of aileron profile on the aerodynamic characteristics of a complete model of a supersonic aircraft configuration

Investigation of dynamic characteristics of a turbine-propeller engine

The effect of thickness ratio on section thrust distribution as determined from a study of wake surveys of the NACA 4-(0)(03)-045 and 4-(0)(08)-045 two-blade propellers up to forward Mach numbers of 0.925

Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 5: analysis and comparison on basis of ram-jet aircraft range and operational characteristics

A comparison of the turbulent boundary-layer growth on an unswept and a swept wing

Theoretical analysis of some simple types of acceleration restrictors

The effects of boundary-layer control on the longitudinal characteristics of a swept-back wing using suction through streamwise slots in the outboard portion of the wing

The effects of centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics of a wing of aspect ratio 10 with 35 degrees of sweepback

The effects of camber and twist on the aerodynamic loading and stalling characteristics of a large-scale 45 degree swept-back wing

Contributions of wing, tail, and fuselage to the aerodynamic characteristics of a semispan model of a supersonic airplane configuration at transonic speeds from tests by the NACA wing-flow method

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