Browse TRAIL Inventories

Flutter analysis of rectangular wings of very low aspect ratio

Some numerical solutions of similarity equations for three-dimensional laminar incompressible boundary-layer flows

Full-scale wind-tunnel tests of a 35 degree sweptback-wing airplane with blowing from the shroud ahead of the trailing-edge flaps

Internal-friction study of aluminum alloy containing 4 weight percent copper

Internal characteristics and performance of several jet deflectors at primary-nozzle pressure ratios up to 3.0

Experimental investigation of flutter and divergence characteristics of the rocket-motor fin of the ASROC missile: COORD. No. N-AM-66

Internal characteristics and performance of an aerodynamically controlled, variable-discharge convergent nozzle

A method for rapid selection of design characteristics of 1-, 1 1/2-, and 2-stage turbines with optimum annulus taper

Investigation of the aerodynamic characteristics of a model of a supersonic bomber configuration with a swept and an unswept wing at Mach numbers from 1.79 to 2.67

Investigation of two-stage counterrotating compressor IV : over-all performance of compressor with modified second-stage rotor

An investigation of supersonic store interference in the vicinity of a 22 degree swept-wing-fuselage configuration at Mach numbers of 1.61 and 2.01

An investigation of some phenomena relating to aural detection of airplanes

A method for the calculation of wave drag on supersonic-edged wings and biplanes

A method for the calculation of the lateral response of airplanes to random turbulence

Exploratory wind-tunnel investigation at high subsonic and transonic speeds of jet flaps on unswept rectangular wings

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

Performance of five short multielement turbojet combustors for hydrogen fuel in quarter-annulus duct

Performance of JP-4 fuel with fluorine-oxygen mixtures in 1000-pound-thrust rocket engines

A nonlinear theory for predicting the effects of unsteady laminar, turbulent, or transitional boundary layers on the attenuation of shock waves in a shock tube with experimental comparison

Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller with an advance ratio of 3.2

Natural convection inside a flat rotating container

Effect of the proximity of the wing first-bending frequency and the short-period frequency on the airplane dynamic-response factor

Preliminary survey of possible methods for hypersonic aircraft

A preliminary study of the effect of boric oxide deposits on the performance of two selected turbine stator-blade shapes

Preliminary transonic flutter investigation of models of T-tail of Blackburn NA-39 airplane

Preliminary heat-transfer studies on two bodies of revolution at angle of attack at a Mach number of 3.12

Effect of leading-edge-flap deflection on the wing loads, load distributions , and flap hinge moments of the Douglas X-3 research airplane at transonic speeds

Preliminary flight survey of fuselage and boundary-layer sound-pressure levels

Procedure for calculating flutter at high supersonic speed including camber deflections, and comparison with experimental results

Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and area-suction flaps

Local isotropy in turbulent shear flow

Longitudinal stability and control characteristics at Mach numbers of 1.41 and 2.01 of a 67 degree swept-wing airplane configuration with canard control surfaces

Local instability of the elements of a truss-core sandwich plate

Low-speed cascade investigation of compressor blades having loaded leading edges

Low-speed experimental determination of the effects of leading-edge radius and profile thickness on static and oscillatory lateral stability derivatives for a delta wing with 60 degrees of leading-edge sweep

Measurement of the effect of an axial magnetic field on the Reynolds number of transition in mercury flowing through a glass tube

Measured and predicted dynamic response characteristics of a flexible airplane to elevator control over a frequency range including three structural modes

Measurements of the motions of a large swept-wing airplane in rough air

Measurements and power spectra of runway roughness at airports in countries of the North Atlantic Treaty Organization

A fuselage addition to increase drag-rise Mach number of subsonic airplanes at lifting conditions

Hypersonic viscous flow over slender cones

Effect of pressure level on afterburner-wall temperatures

Friction studies of various materials in liquid nitrogen

Friction and wear with reactive gases at temperatures up to 1200 F

Free-spinning-tunnel investigation of a 1/28-scale model of the North American FJ-4 airplane: TED No. NACA AD-3112

Heat transfer in isotropic turbulence during the final period of decay

Heat-transfer and pressure measurements on flat-faced cylinders at a Mach number of 2

Heat transfer and thermal stresses in sandwich panels

Comparison of hydrodynamic-impact acceleration and response for systems with single and with multiple elastic modes

Operational problems of manned orbital vehicles


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