Browse TRAIL Inventories

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

Supersonic Wave Interference Affecting Stability

Application of the Method of Coordinate Perturbation to Unsteady Duct Flow

Measurements of free-space oscillating pressures near propellers at flight Mach numbers to 0.72

Turbulent Skin Friction at High Mach Numbers and Reynolds Numbers

Drag minimization for wings and bodies in supersonic flow

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

Characteristics of the Langley 8-foot transonic tunnel with slotted test section

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

Boron and zirconium from crucible refractories in a complex heat-resistant alloy

Prandtl-Meyer expansion of chemically reacting gases in local chemical and thermodynamic equilibrium

Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination

Performance at low speeds of compressor rotors having low-cambered NACA 65-series blades with high inlet angles and low solities

A performance analysis of methods for handling excess inlet flow at supersonic speeds

Rate of reaction of gaseous fluorine with water vapor at 35 degrees C

Stability investigation of a blunt cone and a blunt cylinder with a square base at Mach numbers from 0.64 to 2.14

Performance of a 28-inch ramjet utilizing gaseous hydrogen at a Mach number of 3.6, angles of attack up to 12 degree, and pressure altitudes up to 110,000 feet

Pressure distributions at transonic speeds for parabolic-arc bodies of revolution having fineness ratios of 10, 12, and 14

Pressure distributions at transonic speeds for slender bodies having various axial locations of maximum diameter

Preliminary investigation of graphite, silicon carbide, and several polymer-glass-cloth laminates in a Mach number 2 air jet at stagnation temperatures of 3,000 F and 4,000 F

Preliminary investigation of land-water operation with a 1/10-scale model of a jet airplane equipped with hydro-skis

Stability of propane-air flames in vortex flow

Stagnation-point heat transfer to blunt shapes in hypersonic flight, including effects of yaw

Influence of heat treatment on microstructure and high-temperature properties of nickel-base precipitation-hardening alloy

Analysis of the creep behavior of a square plate loaded in edge compression

Effect of inlet air distortion on steady-state performance of an axial-flow turbojet engine

Effect of inlet aspect ratio on the starting and pressure recovery characteristics of a rectangular swept scoop inlet tested at a Mach number of 3.1

Force and pressure measurements at transonic speeds for several bodies having elliptical cross sections

Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles

Control deflections, airplane response, and tail loads measured on an F-100A airplane in service operational flying

Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively

Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5

Effect of temperature on rolling-contact fatigue life with liquid and dry powder lubricants

Experimental investigation of axial and normal force characteristics of skewed nozzles

Experimental investigation of the effects of some shroud design variables on the static thrust characteristics of a small-scale shrouded propeller submerged in a wing

Experimental investigation of an impulse-type supersonic compressor rotor having a turning of 73 degrees at the mean radius


Published Year

Subject

Author

‹‹ previous 1 2 ... 267 268 269 270 271 272 273 ... 280 281 next ››