Browse TRAIL Inventories

Review of experimental investigations of liquid-metal heat transfer

A reevaluaion of data on atmospheric turbulence and airplane gust loads for application in spectral calculations

A relation between burning velocity and quenching distance

Analysis of cooling-air requirements of corrugated-insert-type turbine blades suitable for a supersonic turbojet engine

Wind-tunnel investigation at low speeds to determine the effect of aspect ratio and end plates on a rectangular wing with jet flaps deflected 85 degrees

Wear of typical carbon-base sliding seal materials at temperatures to 700 F

Weight-flow and thrust limitations due to use of rotating combustors in a turbojet engine

Calculation of the forces and moments on a slender fuselage and vertical fin penetrating lateral gusts

Calculation and compilation of the unsteady-lift functions for a rigid wing subjected to sinusoidal gusts and to sinusoidal sinking oscillations

Temperatures in a J47-25 turbojet-engine turbine section during steady-state and transient operation in an altitude test stand

Comparison between experimental and predicted downwash at a Mach number of 0.25 behind a wing-body combination having a triangular wing of aspect ratio of 2.0

Thermal stability of pentaborane in the range 329 to 419 F

A factor affecting transonic leading-edge flow separation

On slender-body theory and the area rule at transonic speeds

The effects upon body drag of jets exhausting from wing-mounted nacelles

An experimental investigation of a flat ram-jet engine on a helicopter rotor

Gas-turbine-engine performance when heat from liquid-cooled turbines is rejected ahead of, within, or behind main compressor

Gas-to-blade heat-transfer coefficients and turbine heat-rejection rates for a range of one-spool cooled-turbine engine designs

Performance characteristics of ring-cascade-type thrust reversers

Performance of a short combustor at high altitudes using hydrogen fuel

Investigation at high subsonic speeds of some effects of sideslip on the aerodynamic loads on finned and unfinned bodies mounted from the wing of a swept-wing-fuselage model

Investigation at high subsonic speeds of the static lateral and directional stability and tail-loads characteristics of a model having a highly tapered swept wing of aspect ratio 3 and two horizontal-tail positions

Investigation at high subsonic speeds of a body-contouring method for alleviating the adverse interference at the root of a sweptback wing

Effect of fuselage circumferential inlet location on diffuser-discharge total-pressure profiles at supersonic speeds

Effect of three design parameters on the operating characteristics of 75-millimeter-bore cylindrical roller bearings at high speeds

The effects at a Mach number of 6.86 of drag brakes on the lift, drag, and pitching moment of an ogive cylinder

Effects of a J34 turbojet engine on supersonic diffuser performance

Charts for estimating the hovering endurance of a helicopter

Discharge coefficients for combustor-liner air-entry holes

Distribution of losses behind a compressor rotor as measured by a rotating rake

Fatigue crack propagation in severely notched bars

Factors affecting flow distortions produced by supersonic inlets

Fatigue-crack-propagation and residual-static-strength results on full-scale transport-airplane wings

Tests with hydrogen fuel in a simulated afterburner

An experimental study of the zero-angle-of attack transonic drag associated with the vertical position of a horizontal tail at zero incidence

Some experiments relating to the problem of simulation of hot jet engines in studies of jet effects on adjacent surfaces at a free-stream Mach number of 1.80

A theoretical analysis of heat transfer in regions of separated flow

The effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems

Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at Mach numbers from 0 to 1.9

Effect of camber on the drag of a body of revolution

Free-flight investigation at transonic speeds of the stability characteristics of a tailless missile configuration having a 45 degree sweptback wing of aspect ratio 4

Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail

Free-flight investigation at transonic speeds of drag coefficients of a boattail body of revolution with a simulated turbojet exhaust issuing at the base from conical short-length ejectors

A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70

Tensile properties of AZ31A-0 magnesium-alloy sheet under rapid-heating and constant-temperature conditions

Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions

Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7

Comparison of theoretical stresses and deflections of multicell wings with experimental results obtained from plastic models

Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing

Charts adapted from Van Driest's turbulent flat-plate theory for determining values of turbulent aerodynamic friction and heat-transfer coefficients


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