Browse TRAIL Inventories

Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine : over-all performance with standard rotor blading at inlet conditions of 35 inches of mercury absolute and 700 R

A preliminary investigation of methods for improving the pressure recovery characteristics of variable-geometry supersonic-subsonic diffuser systems

Preliminary investigation of combustion of diborane in a turbojet combustor

Preliminary investigation of propane combustion in a 3-inch-diameter duct of inlet-air temperatures of 1400 to 1600 F

Pressure losses of titanium and magnesium slurries in pipes and pipeline transitions

Atmospheric temperature observations to 100,000 feet for several climatological regions of the Northern Hemisphere

Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Influence of crucible materials on high-temperature properties of vacuum-melted nickel-chromium-cobalt alloy

The influence of imperfect radar space stabilization on the final attack phase of an automatic interceptor system

Influence of boric oxide deposition on turbojet-engine operation

Hinge-moment characteristics for a series of controls and balancing devices on a 60 degree delta wing at Mach numbers of 1.61 and 2.01

Development of a piston-compressor type light-gas gun for the launching of free-flight models at high velocity

Effect of hinge-line position on the oscillating hinge moments and flutter characteristics of a flap-type control at transonic speeds

Free-flight experience of the lateral stability characteristics at low lift of a 45 degree swept-wing rocket-propelled model equipped with a nonlinear yaw-rate damper system at Mach numbers from 0.76 to 1.73

Foreign-object retention and flow characteristics of retractable engine-inlet screens

Fatigue Investigation of Full-Scale Transport-Airplane Wings: Variable-Amplitude Tests with a Gust-Loads Spectrum

Accelerations in fighter-airplane crashes

Effect of standing transverse acoustic oscillations on fuel-oxidant mixing in cylindrical combustion chambers

Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests

Hydrogen-oxygen explosions in exhaust ducting

Analog computer study of some filtering, command-computer, and automatic-pilot problems connected with the attack phase of the automatically controlled supersonic interceptor

Experimental investigation of an axial-flow-compressor inlet stage operating at transonic relative inlet Mach numbers V : rotor blade-element performance at a reduced blade angle

Experimental investigation of attenuation of strong shock waves in a shock tube with hydrogen and helium as driver gases

Experimental investigation of performance of single-stage transonic compressor with guide vanes turning counter to direction of rotor whirl

Jet effects on the drag of conical afterbodies for Mach numbers of 0.6 to 1.28

Design and performance of flight-type liquid-hydrogen heat exchanger

Investigation of the effect of velocity diagram on inlet total-pressure distortions through single-stage subsonic axial-flow compressors

Internal performance of several auxiliary air inlets immersed in a turbulent boundary layer at Mach numbers of 1.3, 1.5, and 2.0

Experimental performance of a 5000-pound-thrust rocket chamber using a 20-percent-fluorine-80-percent-oxygen mixture with RP-1

Experimental study of the effects of scale on the absolute values of zero-lift drag of aircraft configurations at transonic speeds

Performance of external-internal compression inlet with abrupt internal turning at Mach numbers 3.0 to 2.0

Preliminary investigation of the combustion of a 50 percent pentaborane - 50 percent JP-4 fuel blend in a turbojet combustor at simulated altitude conditions

Oblique-shock relations at hypersonic speeds for air in chemical equilibrium

Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds

A study of injection processes for liquid oxygen and gaseous hydrogen in a 200-pound-thrust rocket engine

A study of temperature transients at the inlet of a turbojet engine

Preliminary performance evaluation of blends of pentaborate and JP-4 fuel in a full-scale turbojet engine

A review of the physical and thermodynamic properties of boric oxide

Some effects of valve friction and shock stick friction on control quality in a helicopter with hydraulic-power control systems

Thermodynamic study of a Roots compressor as a source of high-temperature air

Thin airfoil theory based on approximate solution of the transonic flow equation

Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with blowing flaps and leading-edge slats

Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with slotted flaps, area-suction flaps, and wing leading-edge devices

Analytical and experimental investigation of the effects of compressor interstage air bleed on performance characteristics of a 13-stage axial-flow compressor

An analysis of vertical-tail loads measured in flight on a swept-wing bomber airplane

Analysis of two-spool turboprop-engine characteristics

Wind-tunnel investigation of the aerodynamic characteristics of a series of swept, highly tapered thin wings at transonic speeds: transonic bumb method

Wind-tunnel investigation of the static lateral stability characteristics of wind-fuselage combinations at high subsonic speeds: Taper-ratio series

Aerodynamic load distribution over a 45 degree swept wing having a spoiler-slot-deflector aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03

Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hydro-ski aircraft with a variable-incidence wing


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