Browse TRAIL Inventories

Wind-tunnel investigation of effects of fuselage cross-sectional shape, fuselage bend, and vertical-tail size on directional characteristics of nonoverlap-type helicopter fuselage models without rotors

On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders

Experimental investigation of the flow around lifting symmetrical double-wedge airfoils at Mach numbers of 1.30 and 1.41

Investigation of the compressive strength and creep lifetime of 2024-T aluminum-alloy skin-stringer panels at elevated temperatures

Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0

Investigation of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy plates at elevated temperatures

Theoretical analysis of linked leading-edge and trailing-edge flap-type controls at supersonic speeds

Gust-load and airspeed data from one type of two-engine airplane on six civil airline routes from 1947 to 1955

An experimental investigation of the scale relations for the impinging water spray generated by a planing surface

Experimental investigation of the vibrations of a built-up rectangular box beam

Particular solutions for flows at Mach number 1

Flow studies on drooped-leading-edge delta wings at supersonic speed

Effect of shallow water on the hydrodynamic characteristics of a flat-bottom planing surface

A Transonic Wind-Tunnel Investigation of a Seaplane Configuration having a 40 Deg Sweptback Wing, TED No. NACA DE 387

Aerodynamic design of axial-flow compressors: Volume 3

Friction, wear, and surface damage of metals as affected by solid surface films

Intensity, scale, and spectra of turbulence in mixing region of free subsonic jet

Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees

Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition

The near noise field of static jets and some model studies of devices for noise reduction

Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data

A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition

On the Kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow

Effect of chord size on weight and cooling characteristics of air-cooled turbine blades

Static Longitudinal and Lateral Stability and Control Data Obtained from Tests of a 1/15-Scale Model of the Goodyear XZP5K Airship, TED No. NACA DE 211

Hovering-flight tests of a model of a transport vertical-take-off airplane with tilting wing and propellers

Component performance investigation of J71 experimental turbine I : over-all performance with 97-percent-design stator areas

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


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