27th Aerospace Sciences Meeting 1989
DOI: 10.2514/6.1989-49
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Separated-flow considerations for pressure-atomized combusting monopropellant sprays

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(16 citation statements)
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“…19 The pressure of the combusting spray was set by adjusting the initial pressure of the combustible gas mixture because combustion of this gas approximated a constant volume process. 3 The adiabatic combustion temperature of the gas mixture was somewhat greater than the adiabatic constantpressure combustion temperature of the monopropellant (see Table 1); however, temperature variations in this range do not have a large effect on drop burning rates. 3 Additionally, these combustion gas temperatures are representative of conditions in liquid guns where combustion temperatures are increased due to constant volume combustion.…”
Section: Apparatusmentioning
confidence: 89%
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“…19 The pressure of the combusting spray was set by adjusting the initial pressure of the combustible gas mixture because combustion of this gas approximated a constant volume process. 3 The adiabatic combustion temperature of the gas mixture was somewhat greater than the adiabatic constantpressure combustion temperature of the monopropellant (see Table 1); however, temperature variations in this range do not have a large effect on drop burning rates. 3 Additionally, these combustion gas temperatures are representative of conditions in liquid guns where combustion temperatures are increased due to constant volume combustion.…”
Section: Apparatusmentioning
confidence: 89%
“…Motivated by these considerations, the present investigation considered the structure of combusting pressureatomized monopropellant sprays both theoretically and experimentally, seeking to extend earlier work in this laboratory. 1 " 3 Similar to the earlier studies, r~3 the investigation was limited to a hydroxylammonium nitrate (HAN)-based monopropellant (LGP 1845) which is of interest for several highpressure monopropellant combustion systems.…”
Section: Nomenclaturementioning
confidence: 95%
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