TRAIL - Technical Report Archive and Image Library

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

Analytical investigation of the effect of water injection on supersonic turbojet-engine - inlet matching and thrust augmentation

Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion

Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine

Cascade investigation of cooling characteristics of a cast-finned air-cooled turbine blade for use in a turboprop engine

A comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies

Comparison of calculated and experimental load distributions on thin wings at high subsonic and sonic speeds

Comparison of effect of a turbojet engine and three cold-flow configurations on the stability of a full-scale supersonicle inlet

Combustor performance of a 16-inch ram jet using gaseous hydrogen as fuel at Mach number 3.0

An analytical investigation of the gust-alleviating properties of a simple pitch damper

Analysis of operational airline data to show the effects of airborne weather radar on the gust loads and operating practices of twin-engine short-haul transport airplanes

Flight tests of a model of a high-wing transport vertical-take-off airplane with tilting wing and propellers and with jet controls at the rear of the fuselage for pitch and yaw control

Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade

Analysis of experimental low-speed loss and stall characteristics of two-dimensional compressor blade cascades

Analysis of fluorine addition to the vanguard first stage

Analysis of horizontal-tail loads in pitching maneuvers on a flexible swept-wing jet bomber

Characteristics of a 40 degree cone for measuring Mach number, total pressure, and flow angles at supersonic speeds

The combinations of thermal and load stresses for the onset of permanent buckling in plates

Comparison of experimental with theoretical total-pressure loss in parallel-walled turbojet combustors

Component performance investigation of J71 experimental turbine VII: effect of first-stator adjustment; over-all performance of J71 turbine with 87-percent-design stator area

Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number

Bonded lead monoxide films as solid lubricants for temperatures up to 1250 F

Boundary-layer transition at Mach 3.12 as affected by cooling and nose blunting

Effect of overheating on creep-rupture properties of S-816 alloy at 1,500 F

Expected numbers of maxima and minima of a stationary random process with non-Gaussian frequency distribution

Experimental and calculated histories of vaporizing fuel drops

Wind-tunnel technique for simultaneous simulation of external flow field about nacelle inlet and exit airstreams at supersonic speeds

Design and experimental evaluation of a light-weight turbine-wheel assembly

Effects of leading-edge blunting on the local heat transfer and pressure distributions over flat plates in supersonic flow

The effect of forward-flight speed on the propulsive characteristics of a pulse-jet engine mounted on a helicopter rotor

Effect of frequency and temperature on fatigue of metals

Effect of propeller location and flap deflection on the aerodynamic characteristics of a wing-propeller combination for angles of attack from 0 degrees to 80 degrees

Effects of thermal relaxation and specific-heat changes on measurements with a pneumatic-probe pyrometer

Experimental investigation of several afterburner configurations on a J79 turbojet engine

The use of pure twist for drag reduction on arrow wings with subsonic leading edges

Estimation of compressible boundary-layer growth over insulated surfaces with pressure gradient

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