Maximum drop diameters for the atomization of liquid jets injected concurrently into accelerating or decelerating gas streams
Maximum drop diameters for atomization of liquid jets injected concurrently into accelerating or decelerating gas streams
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Maximum drop diameters for atomization of liquid jets injected concurrently into accelerating or decelerating gas streams
Preliminary analysis of three impulse technique for transearth injection from highly inclined orbits
Film cooling effectiveness with gas injection through discrete orifice into turbulent boundary layer in subsonic wind tunnel
Combustion performance of liquid rocket engine studied in presence of several near-wall injection conditions
Performance of vortex valve controlled secondary injection thrust vector system for solid propellant rocket motor control
Initial air boundary layer effect on ignition of slot-injected gaseous hydrogen in supersonic airstream, discussing isotherm and streamline patterns
Drag reduction in turbulent pipe flow of Newtonian fluid through injection of additives
Nitrogen injection on blunt reentry body, investigating influence on separation, transition, static stability and control effectiveness
Injection lasers of gallium arsenic phosphide alloys studied for threshold current densities and emission efficiency
Experiments to determine film cooling with air injection through holes into turbulent air boundary layer on flat plate
Pathophysiologic effects of oxygen emboli injected into right heart and pulmonary artery, discussing autonomic blocking agent
Gallium arsenide injection lasers, discussing external cavity coupling, phase locking, laser uniformity, dimensions and arrays
Solar flare injection and propagation of low energy protons and electrons in 7-9 July 1966 solar particle event
Quasi-optimum steering law for minimum time orbital injection rocket booster
Hydrogen filled Saturn 2 injection stage assembled with flyby mission spacecraft in earth orbit for Mars/Venus flyby mission
Douglas Anchored Interplanetary Monitoring Platform-E real time system operation during translunar flight for in-flight determination of lunar orbit injection conditions
To prevent samples containing foreign matter from poisoning the gas chromatographic columns, a pre-filter insertion is placed in the injection port. The packing becomes a variable reactant, for example, acids are removed by using an alkaline liquid.
Correlation equation on entrainment-viscosity behavior in cryogenic tank during gas injection