TRAIL - Technical Report Archive and Image Library

Low-speed measurements of tail contribution to rolling stability derivatives and air-flow angularity at the tail for an x-tail model in steady roll including some effects of wing-tip stores

Low-speed investigation of the lateral-control characteristics of a flap-type spoiler and a spoiler-slot deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section

Low-Speed Static Stability Characteristics of a Complete Model with an M-Wing in Mid and High Positions and with Three Horizontal-Tail Heights

Low-speed wind-tunnel results for a thin aspect-ratio-1.85 pointed-wing-fuselage model with double slotted flaps

Methods for measuring temperatures of thin-walled gas-turbine blades

Methods for calculating thrust augmentation and liquid consumption for various turbojet-afterburner fuels

Minimum-drag ducted and closed three-point body of revolution based on linearized supersonic theory

Minimum drag of the Chance Vought XF8U-1 airplane as determined from the flight test of a 0.11-scale rocket-boosted model at Mach numbers between 0.73 and 1.71 : TED No. NACA DE 392

Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance

Poisson's ratios and volume changes for plastically orthotropic material

Seat design for crash worthiness

Some considerations regarding the application of the supersonic area rule to the design of airplane fuselages

Perforated sheets as a porous material for distributed suction and injection

Performance characteristics of an axial-flow transonic compressor operating up to tip relative inlet Mach number of 1.34

Performance characteristics of cylindrical target-type thrust reversers

Rapid determination of core dimensions of crossflow gas-to-gas heat exchangers

Radiation and recovery corrections and time constants of several chromel-alumel thermocouple probes in high-temperature, high-velocity gas streams

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

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

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