Browse TRAIL Inventories

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

Aerodynamic performance of several techniques for spike-position control of a blunt-lip nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to 2.0

Aerodynamic characteristics at Mach number of 4.06 of a typical supersonic airplane model using body and vertical-tail wedges to improve directional stability

An experimental hydrodynamic investigation of the inception of vortex ventilation

Effects of rapid heating on strength of airframe components

Generalized master curves for creep and rupture

Experimental evaluation of 'swirl-can' elements for hydrogen-fuel combustor

Experimental influence coefficients and vibration modes of a built-up 45 degree delta-wing specimen

Free-flight performance of a rotating-vane-spoiler roll control system with low actuating forces

Hydrodynamic investigation of a model of a supersonic multijet water-based aircraft with engines exhausting from the step

Investigation of an afterburning ramjet using gaseous hydrogen as fuel at Mach number of 3.0

Investigation of an underslung scoop inlet at Mach numbers to 1.99

Investigation of axially symmetric flow over steps at transonic speeds with comparisons of estimated and experimental drag results

Investigation of an underslung normal-wedge inlet at free-stream Mach numbers from 1.50 to 1.99

Cooling performance and structural reliability of a modified corrugated-insert air-cooled turbine blade with an integrally cast shell and base

Static strength of cross-grain 7075-T6 aluminum-alloy extruded bar containing fatigue cracks

Effect of spanwise variations in gust intensity on the lift due to atmospheric turbulence

A collection of data for zero-lift damping in roll of wing-body combinations as determined with rocket-powered models equipped with roll-torque nozzles

Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0

Effects of extreme surface cooling on boundary-layer transition

A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed

Effect of interstage bleed on rotating stall and blade vibration in a 13-stage axial-flow compressor in a turbojet engine

The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections


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