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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Electrical noise measurement system measures noise generated by edge-type connectors and circuit cards when they are subjected to sinusoidal vibration. It provides a signal across the contact area and monitors the signal change during vibration. Noise measured can be expressed as a varying change in total contact resistance.
Problem of determining hidden edges of computer drawn convex polyhedra
Vibration analysis of cylindrically curved panels with simply supported or clamped edges
Edge diffraction from truncated parabolic and hyperbolic reflectors
Elastic displacements for various edge-cracked plate specimens using boundary collocation computing procedures
Stress intensity analysis for flat plates loaded close to edge crackline, giving intensity dependence on crack length and specimen shape
Numerical data for plane thermal stresses in isotropic elastic square plate bounded by edge stiffeners and under symmetric temperature distributions
FORTRAN 4 program for computerized design of two dimensional supersonic nozzles with sharp edged throats
Transverse edge effect in plane induction magnetohydrodynamic generators
Longitudinal edge effect in linear induction magnetohydrodynamic generators
Static pressure and flow field for flat plate model with short trailing-edge flap
Plane stress analysis using Fourier series of edge stiffened isotropic or orthotropic elastic rectangular plate subjected to prescribed temperature distribution and boundary loads
Laminar flow separation on flat plate induced by deflected trailing-edge flap at hypersonic speed
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer separation at moderate enthalpies in hypersonic flow
Effects of edge constraints on optical qualities of Gemini spacecraft windows
Hypersonic flow distribution and separation types over highly swept delta wings with trailing edge flaps at Mach 6
Electromagnetic field behavior near conducting wedge edge in contact with uniaxial plasma, noting intrinsic loss without surface waves
Edge constraint effect on buckling of sandwich and ring stiffened conical shells under external pressure