Enhanced grain boundary sliding during reversed creep of lead
Grain boundary migration in lead after repeated creep stress reversals
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Grain boundary migration in lead after repeated creep stress reversals
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.4
Design and tests of thermoelectric systems with germanium silicon or lead telluride
Biomedical ground lead system with high voltage and pinch-off FETs, and one resistor for limiting current flow
Aluminum-contacted lead telluride thermoelectric test modules in life testing
Cooling and structural performance of hypersonic research engine cowl leading edge
Lead isotope composition and concentrations of U, Th, Ra, total Pb and Pb 210 in recent volcanic rocks, noting disequilibrium due to chemical fractionations
Chemical compatibility estimation of lead and tin tellurides thermoelectric materials with metallic alloys
Kinetic theory of sharp leading edge parallel to supersonic flow using Boltzmann equation, determining flow field
Boltzmann equation with BGK model as governing equation for sharp leading edge problem in supersonic flow
Supersonic leading edge problem using nonlinear Boltzmann equation with ellipsoidal model, calculating molecular distribution functions for flow field
Results are presented of a free-flight investigation between Mach numbers of 0.7 to 1.3 and Reynolds numbers of 3.1 x 10(exp 6) to 7.0 x 10(exp 6) to determine the longitudinal aerodynamic characteristics of the Northrop MX-775A missile. This missile has a weng, body, and vertical tail, but has no horizontal tail. The basic wing plan form has an aspect ratio of 5.5, 45 deg of sweepback of the 0.406 streamwise chord line, and a taper ratio of 0.4. A 1/10-scale steel-wing model of the missile was flown with modifications to the basic wing plan form consisting of leading-edge chord-extensions deflected 7 deg downward together with the forward 15 percent of the wing chord, and inboard trailing-edge flaps deflected 5 deg downward. In addition, the model had a static-pressure tube mounted at the tip of the vertical tail for position-error measurements and had a speed brake also mounted on the vertical tail to trim the model to positive lift coefficients and to permit determination of the trim and drag effectiveness of the brake. The data are uncorrected for the effects of wing elasticity, but experimental wing influence coefficients are presented.
Tool bends leads quickly and accurately for mounting on printed circuit boards. It has grooves and bend-angles aligned for particular circuit board applications.
Electron microprobe study of inclusions in lead telluride thermoelectric elements
Investigation of fluctuation and correlation in electromagnetic and nuclear showers developing in lead
Thermoelectric system of Cd-Si-Ge, and tungsten diffusion bonded lead telluride
Finite difference solution for compressible turbulent boundary layer equations of swept slab with leading edge blowing
FORTRAN 4 program for nonconical flow past slender wing bodies with leading edge separation