Transonic aerodynamic characteristics of a medium hypersonic LD reentry spacecraft with a variable geometry wing
Transonic aerodynamic characteristics of variable geometry reentry vehicle with hypersonic lift drag ratio
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Transonic aerodynamic characteristics of variable geometry reentry vehicle with hypersonic lift drag ratio
Reaction geometry in oxidation and reduction of alkaline silver electrode
Variable geometry inlet guide vanes and stators for extending stable operation of supersonic cruise turbine engine compressor front stage
Parametric design study of self-acting pad geometries for shaft seals in turbocompressors
Fixed geometry wind tunnel model of auxiliary inlet ejector with clamshell flow diverter from Mach 0 to 1.2
Electron microscopic studies of reaction geometry in oxidation and reduction of alkaline silver electrodes
Probe geometry effects on hot film anemometer probe performance during turbulence measurements in liquids
Liquid rocket engine injector elements design criteria, using noncircular orifice geometry to predict efficiency
Mercury electron bombardment thrustor, measuring effect of geometry and magnetic field inside pole piece region on discharge losses and propulsion efficiency
Computer program calculates trajectories of orbiting spacecraft and lander vehicles simultaneously. Using data from both vehicles, program calculates communications geometry which consists of orbiting spacecraft cone/clock angle, lander cone/clock angle, range, range rate and acceleration, and fade, reflective, and system margins.
Jovian magnetic field geometry and Io modulated decametric radio emission
Variable geometry manned orbital vehicle having high aerodynamic efficiency over wide speed range and incorporating auxiliary pivotal wings
Developing empirical equation for calculating effects of container geometry on liquid lubricant evaporation in vacuum
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for two stage axial flow turbine
Booster wing geometry effects on space shuttle design requirements
Inlet nozzle geometry effects on subsonic flow characteristics of miniature total pressure tubes including pitot tube static and dynamic pressure and flow velocity measurements
Low speed wind tunnel test on effects of horizontal tail geometry on longitudinal stability of orbiter shuttle
Low speed wind tunnel tests on effects of vertical tail and geometry on directional stability of orbital space shuttle model