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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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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
Electron radiation effect on open geometry p channel enhancement type MOSFET gate threshold voltage, noting peaking anomaly
Cylindrical geometry thermionic converter with vapor deposited W emitter, noting power density performance characteristics, work function and long term stability
Single highest peak /SHP/ maximum response to random noise excitation of distributed elastic structures with rectangular geometry, considering beam and flat plate
Variable geometry supersonic aircraft design, discussing inlet and exhaust nozzles problems and wind tunnel tests
Computer program determines the alternative geometries and associated design point performance of axial-flow turbines capable of satisfying specified design requirements. The program solves the flow field within the turbine without making the simplifying assumptions that result in restrictive designs.
Generation of near encounter spacecraft-target planet celestial geometry using two body trajectory computerized simulation
Minimization of optical resonance scattering by adjustment of monochromator slit geometry
Hypersonic aerodynamic characteristics of low fineness ratio variable geometry logistics spacecraft model
Inlet flow distortion effects on single stage variable geometry guide vanes and stators
Plug and shroud geometry variables on plug nozzle performance at transonic speeds
Injector radial distribution and thrust chamber geometry effect on acoustic mode instability in hydrogen oxygen engines
Variable geometry features applied to lifting spacecraft to overcome inherent incompatibility and provide low speed and tangential landing capabilities
Aerodynamic and flight characteristics of variable geometry entry spacecraft during subsonic wing deployment and landing
Gas core reactor curved porous walls geometry tested with clear and smoky air injection, noting mass flow ratio in reactor cavity
Computer programming for graphic display of combinatorial geometry