TRAIL - Technical Report Archive and Image Library

Ditching investigations of dynamic models and effects of design parameters on ditching characteristics

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study 3: experimental performance with two stator configurations designed to eliminate blade wakes and secondary-flow effects and conclusions from entire sta

Performance of a supersonic ramp-type side inlet with ram-scoop throat bleed and varying fuselage boundary-layer removal : Mach number range 1.5 to 2.0

Permeability variation of a taper-rolled wire cloth

A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures

Investigation at low speeds of deflectors and spoilers as gust alleviators on a model of the Bell X-5 airplane with 35 degree swept wings and on a high-aspect-ratio 35 degree swept-wing-fuselage model

Investigation of conditions for spontaneous ignition and combustion efficiency of pentaborane in a small-scale combustor

Charts for estimating the effects of short-period stability characteristics on airplane vertical-acceleration and pitch-angle response in continuous atmospheric turbulence

Effect of fuselage length and a canopy on the static longitudinal and lateral stability characteristics of 45 degrees sweptback airplane models having fuselages with square cross sections

The effect of body contouring on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail and several wing-fuselage combinations having sweptback wings of relatively high aspect ratio

Effect of burner design variables on performance of 16-inch diameter ram-jet combustor using gaseous-hydrogen fuel

Fatigue-crack propagation and residual static strength of built-up structures

An investigation of discharge and thrust characteristics of flapped outlets for stream Mach numbers from 0.40 to 1.30

Charts for the analysis of flow in a whirling duct

Investigation of effectiveness of a wing equipped with a 50-percent-chord sliding flap, a 30-percent-chord slotted flap, and a 30-percent-chord slat in deflecting propeller slipstreams downward for vertical take-off

External interference effects of a flow through static-pressure orifices of a NACA airspeed head at a Mach number of 3

Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality

Experimental investigation of the simulation of atmospheric entry of ballistic missiles

Effects of airplane flexibility on wing bending strains in rough air

The effects of boundary-layer separation over bodies of revolution with conical tail flares

Effects of airplane flexibility on wing strains in rough air at 5,000 feet as determined by flight tests of a large swept-wing airplane

Effects of blade plan form on free-space oscillating pressures near propellers at flight Mach numbers to 0.72

Free-flight investigation of jet effects at low supersonic Mach numbers on a fighter-type configuration employing a tail-boom assembly: longitudinal stability and trim

Exploratory study of ground proximity effects on thrust of annular and circular nozzles

Results of the flight test of a 0.13-scale rocket-boosted model of the McDonnell F4H-1 airplane between Mach numbers of 0.20 and 1.90: TED No. NACA AD 3115

Flight tests of an automatic interceptor system with a tracking radar modified to minimize the interaction between antenna and interceptor motions

Exploratory investigation of aerodynamic effects of external combustion of aluminum borohydride in airstream adjacent to flat plate in Mach 2.46 tunnel

Full-scale free-jet investigation of a two-shock side-inlet diffuser at Mach 2.75 and a comparison with a single-shock diffuser

Impact-loads investigation of chine-immersed models having concave-convex transverse shape and straight or curved keel lines

Impact-loads investigation of a chine-immersed model having a longitudinally curved bow and a v-bottom with a dead-rise angle of 30 degrees

Heat transfer and boundary-layer transition on two blunt bodies at Mach numbers 3.12

Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15

Heat-exchanger-core weights for use with hydrogen expansion turbine

The heat of combustion of tetraethyldiborane

A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61

Investigation of a nonlinear control system

Preliminary investigation of the characteristics of a two dimensional wing and propeller with the propeller plane of rotation in the wing-chord plane

Investigation of a nonlinear control system

Recent research on the creep of airframe components

Applications of power spectral analysis methods to maneuver loads obtained on jet fighter airplanes during service operations

Effect of fiber orientation on ball failures under rolling-contact conditions

Effect of crystal orientation on fatigue-crack initiation in polycrystalline aluminum alloys

Arrangements of jet engine and airframe for increased range

Effect of fuel properties on liner temperatures in a single tubular turbojet combustor

Creep behavior of structural joints of aircraft materials under constant loads and temperatures

Creep deformation patterns of joints under bearing and tensile loads

Drop burning rates of hydrocarbon and nonhydrocarbon fuels

Effect of lubricant viscosity on rolling-contact fatigue life

Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94

Effect of overheating on creep-rupture properties of HS-31 alloy at 1,500 F

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