The measurement of superparamagnetic particle shapes and size distribution
Measurement of superparamagnetic particle shapes and size distribution
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Measurement of superparamagnetic particle shapes and size distribution
Velocity, Bond number and Weber number effects on liquid free surface shape and meniscus height under reduced gravity
Paraglider wing analysis based on assumption that its flexibility allows it to take shape that aerodynamic pressure and internal stresses dictate
Shock front shape perturbations due to boundary layer effects and shock tube and piston imperfections
Liquid-gas interface shape in cylindrical rocket tanks under reduced gravity
Propagating tensile fracture of constant ellipse shape treated as steady state dynamic mixed boundary value problem
A study has been made of a flare-cylinder configuration to investigate its feasibility as a reentry body of an intermediate range ballistic missile. Factors considered were heating, weight, stability, and impact velocity. A series of trajectories covering the possible range of weight-drag ratios were computed for simple truncated nose shapes of varying pointedness, and hence varying weight-drag ratios. Four trajectories were chosen for detailed temperature computation from among those trajectories estimated to be possible. Temperature calculations were made for both "conventional" (for example, copper, Inconel, and stainless steel) and "unconventional" (for example, beryllium and graphite) materials. Results of the computations showed that an impact Mach number of 0.5 was readily obtainable for a body constructed from conventional materials. A substantial increase in subsonic impact velocity above a Mach number of 0.5 was possible without exceeding material temperature limits. A weight saving of up to 134 pounds out of 822 was possible with unconventional materials. This saving represents 78 percent of the structural weight. Supersonic impact would require construction of the body from unconventional materials but appeared to be well within the range of attainability.
Welded steel clamps securely grip structural shapes of various sizes for crane operations. The clamp has adjustable clamping jaws and screw-operated internal v-jaws and provides greater safety than hoisting slings presently used. The structural member can be rotated in any manner, angle, or direction without being released by the clamp.
Computer program evaluates heat transfer modes and calculates either the transient or steady-state temperature distributions throughout an object of complex shape when heat sources are applied to specified points on the object. It uses an electrothermal model to simulate the conductance, heat capacity, and temperature potential of the object.
Wind tunnel measurements on effect of slender body shape on sonic boom pressure distributions
Rectangular distributed RC network consisting of resistive layer separated by insulator from three shaped electrodes
Equilibrium shape of radio astronomy satellite antenna array in circular orbit
Mapping function derivation for large class of star-shaped regions by Schwarz-Christoffel transformation
Casting, powder metallurgy, electroforming, metal spraying, and chemical vapor deposition techniques for producing nickel and nickel-alloy shapes
Flight characteristics of free flying aerodynamically shaped balloons
Making titanium and titanium shapes by casting, powder metallurgy, metal spraying, vapor deposition, and electroforming
Viscous flow and nose inlet shape effects on pitot tube pressure measurements
Precision winding of cylindrical composites with shaped glass filaments - mechanical property determination