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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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Activation growth, and detachment of boiling bubbles in water from artificial nucleation sites of known geometry and size drilled in polished metal surface
Mach number and geometry effects on level of sonic boom overpressure and applicability of Whitham theory to calculation of sonic boom
Groove geometry effect on performance viscoseal with sealed water in laminar and turbulent conditions
Incipience, growth and detachment of boiling bubbles in saturated distilled water from artificial nucleation sites of given geometry and size in heated metal surface
Materials and fin tube geometry effects on ultimate size and mass of space radiator
Groove geometry effect on performance viscoseal with sealed water in laminar and turbulent conditions
Similarity parameters used for examining geometry characteristics of axial flow turbines with high expansion ratio
Space orientated supplement to secondary level geometry textbooks
Optimum design geometry for high radial inflow turbine performance efficiency
Weight, heat transfer, and efficiency comparison for Rankine cycle space radiators constructed of three different finned tube geometries
Tabular and graphical data geometry and dynamics of earth-moon-sun system for 1966-1985 time period
Variable geometry concepts applied to guide vanes and stators in single stage compressors
Plasma instability onset and suppression in crossed field geometry controlled by radial magnetic field near cathode
Reaction geometry effects on oxidation and reduction of alkaline silver electrodes
Variable geometry requirements in exhaust nozzles and inlets for high Mach number applications
Effects of electrolyte amount, drain rate, and electrode geometry on copper oxide-magnesium thermal cell performance
Nose shape and fin geometry effects on static stability of sounding rocket models in supersonic wind tunnel
Windshield and nose geometry effects on supersonic aerodynamic characteristics of tactical fighter model