Browse TRAIL Inventories

Some effects of ailerons on the variation of aerodynamic characteristics with sideslip at low speed

Some considerations of the influence of body cross-sectional shape on the lifting efficiency of wing-body combinations at supersonic speeds

Some aspects of supersonic inlet stability

Pressure distributions and aerodynamic characteristics of several spoiler-type controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01

Preliminary flight survey of aerodynamic noise on an airplane wing

Preliminary investigation of self-excited vibrations of single planing surfaces

Preliminary investigation of Guy alloy as a turbojet-engine bucket material for use at 1650 degrees F

Stability of supersonic inlets at Mach 1.91 with air injection and suction

Attenuation of tangential-pressure oscillations in a liquid-oxygen - n-heptane rocket engine with longitudinal fins

Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80 degree delta-wing missile

Calculations of the flow over an inclined flat plate at free-stream Mach number 1

Average properties of compressible laminar boundary layer on flat plate with unsteady flight velocity

Experimental determination of the range of applicability of the transonic area rule for wings of triangular plan form

Effect of inlet-air-flow-distortions on steady-state performance of J65-B-3 turbojet engine

Effect of inlet-duct length in uniform-flow field on turbojet-engine operation

Effect of increase in angle of dead rise on the hydrodynamic qualities of a seaplane configuration incorporating high wing loading

The influence of surface injection on heat-transfer and skin friction associated with the high-speed turbulent boundary layer

Design of two transpiration-cooled strut-supported turbine rotor blades

Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds

Afterburner performance with combustion-chamber lengths from 10 to 62 inches at several afterburner-inlet temperatures

An analog study of the relative importance of various factors affecting roll coupling

Experimental investigation of an overriding control to effect recovery from surge and stall in a turbojet engine

Jet effects on base and afterbody pressures of a cylindrical afterbody at transonic speeds

Investigation of the effects of body camber and body indentation on the longitudinal characteristics of a 60 degree delta-wing-body combination at a Mach number of 1.61

A method for calculation of free-space sound pressures near a propeller in flight including considerations of the chordwise blade loading

Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow

Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow

Low-speed longitudinal stability and lateral-control characteristics of a model of a 40 degree swept-wing fighter-type airplane at a Reynolds number of 9 x 10(exp 6)

Preliminary investigation of short two-dimensional subsonic diffusers

Preliminary investigation of the effects of external wing fuel tanks on ditching behavior of a sweptback-wing airplane

Observation of laminar flow on a blunted 15 degree cone-cylinder in free flight at high reynolds numbers and free-stream mach numbers to 8.17

Some effects of joint conductivity on the temperatures and thermal stresses in aerodynamically heated skin-stiffener combinations

Temperature-control study of turbine region of turbojet engine, including turbine-blade time constants and starting characteristics

Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds

Preliminary report on a study of separated flows in supersonic and subsonic streams

Some effects of guide-vane turning and stators on the rotating stall characteristics of a high hub-tip ratio single-stage compressor

Some effects of small-scale flow disturbance on nozzle-burner flames

Thermodynamic study of air-cycle and mercury-vapor-cycle systems for refrigerating cooling air for turbines or other components

Three-dimensional transonic flow theory applied to slender wings and bodies

Thermodynamic properties of products of combustion of hydrogen with air fo r temperatures of 600 to 4400 R

Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 : supplement I- influence of new boric-oxide vapor-pressure data on calculated performanc

Analysis of turbomachine viscous losses affected by changes in blade geometry

Analysis of turbojet-engine controls for afterburning starting

Analysis of the vertical-tail loads measured during a flight investigation of the Douglas X-3 research airplane

The appearance of a boric oxide exhaust cloud from a turbojet engine operating on trimethylborate fuel

Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of plain spoilers on thin untapered wings at transonic speeds

Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bump method

Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds: taper-ratio series

Theoretical lift due to wing incidence of slender wing-body-tail combinations at zero angle of attack

Visualization of rotor tip secondary flows with blade tip air discharge and suction in a low-speed turbine


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