Add to ORKGBurning solid aluminum and magnesium spheres in high temperature and high velocity gases by combustion of hydrogen and oxyge
Micron-sized metal powders carried by a nitrogen flow were fed along the axis of a cylindrical hydro...
Combustible metal dust explosions continue to present a significant threat to metal handling and ref...
It is common practice to add reactive metal particles to high-explosive formulations ...
The ignition and combustion of Al, Mg, and Al/Mg alloy particles in 99 percent O2/1 percent N2 mixtu...
Metal additives have been widely used in combustion applications such as solid rocket motors and hig...
Recent interest in developing Al-Mg alloys as reactive materials prompted studies of combustion mech...
Predictive mechanisms for particle ignition and combustion rates are required in order to develop op...
The paper presents a physical-mathematical model for metallized solid propellant combustion under ac...
A study of the high-temperature oxidation of several aircraft construction materials was undertaken ...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
NASA determines flammability of metal and alloy samples in high pressure oxygen by Test 17 of NHB 80...
This annual report summarizes the latest results obtained in a NASA-supported project to investigate...
The combustion of metals is a field with important practical applications in rocket propellants, hig...
Aluminum size and loading effects on burning rate of centrifugal accelerated solid propellant
Micron-sized metal powders carried by a nitrogen flow were fed along the axis of a cylindrical hydro...
Combustible metal dust explosions continue to present a significant threat to metal handling and ref...
It is common practice to add reactive metal particles to high-explosive formulations ...
The ignition and combustion of Al, Mg, and Al/Mg alloy particles in 99 percent O2/1 percent N2 mixtu...
Metal additives have been widely used in combustion applications such as solid rocket motors and hig...
Recent interest in developing Al-Mg alloys as reactive materials prompted studies of combustion mech...
Predictive mechanisms for particle ignition and combustion rates are required in order to develop op...
The paper presents a physical-mathematical model for metallized solid propellant combustion under ac...
A study of the high-temperature oxidation of several aircraft construction materials was undertaken ...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
NASA determines flammability of metal and alloy samples in high pressure oxygen by Test 17 of NHB 80...
This annual report summarizes the latest results obtained in a NASA-supported project to investigate...
The combustion of metals is a field with important practical applications in rocket propellants, hig...
Aluminum size and loading effects on burning rate of centrifugal accelerated solid propellant
Micron-sized metal powders carried by a nitrogen flow were fed along the axis of a cylindrical hydro...
Combustible metal dust explosions continue to present a significant threat to metal handling and ref...
It is common practice to add reactive metal particles to high-explosive formulations ...