Transient burning of spherical symmetric fuel droplets.
Spherical symmetric unsteady conservation equations describing transient burning of volatile fuel droplets, obtaining time dependent fuel and heat distribution in flow field
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.
Spherical symmetric unsteady conservation equations describing transient burning of volatile fuel droplets, obtaining time dependent fuel and heat distribution in flow field
Elements nucleosynthesis during thermonuclear burning of carbon at series of temperatures and for several initial compositions
Burning solid propellant behavior under pressure fluctuations expressed in response function terms defining small mass flux change ratio to small pressure change
Supercritical burning of liquid fuel droplets in stagnant environment, using flame sheet model to obtain heat and mass fields
Atmospheric selection and gravity effects on burning rate and ignition temperature
Elementary physical model for flammable materials combustion emphasizing downward burning
Effects of acceleration and gas composition on burning rate of spacecraft materials
Effects of acceleration on burning rate of spacecraft materials
Liquid rocket propellant droplet burning rate and lifetimes in combustion chamber
Experimental droplet burning rates obtained at atmospheric pressure in combustion gas environment
Stability limits and efficiency of swirl can combustor modules burning natural gas fuel
Finite and impulsive burn simulations of fixed attitude translunar injection aborts
Manual completion of lunar orbit insertion burn with inertial measuring unit drifting about pitch axis
Feasibility of manual completion of LOI burn with body mounted attitude gyro drifting about pitch axis
Burning solid aluminum and magnesium spheres in high temperature and high velocity gases by combustion of hydrogen and oxygen
Position control of burning solid nonmetallized propellant strand in combustion bomb using closed loop servomechanism
BeO whiskers formation on burning Be droplets surface using scanning electron microscopy, noting temperature effects
Shooting method for real time optimization of multiple burn rocket flights, presenting analysis, algorithm and test results