2020
DOI: 10.1016/j.combustflame.2020.04.011
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Radiation heat transfer in ablating boundary layer combustion theory used for hybrid rocket motor analysis

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Cited by 23 publications
(11 citation statements)
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“…Figure 1a shows the 2D slab burner experiment for paraffin wax-gaseous oxygen hybrid combustion. The experiments are conducted in the setup that is based on [4] and [15]. The experiment uses solid paraffin wax (or candle wax) as the fuel because of its low cost and high regression rate characteristics.…”
Section: Methodsmentioning
confidence: 99%
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“…Figure 1a shows the 2D slab burner experiment for paraffin wax-gaseous oxygen hybrid combustion. The experiments are conducted in the setup that is based on [4] and [15]. The experiment uses solid paraffin wax (or candle wax) as the fuel because of its low cost and high regression rate characteristics.…”
Section: Methodsmentioning
confidence: 99%
“…Hybrid rockets are recently gaining attention and becoming a competitive propulsion system because they have the benefits of solid and liquid rockets in one platform [17,24]. The fuel and oxidizer are in two different states: typically the fuel is a solid and the oxidizer is a gas/liquid, providing a highly dense fuel source similar to a bi-propellant solid motor but with the throttle control of a liquid motor [4,10,28]. The fuel regression rate ( ṙ) corresponds to the rate that the fuel recedes over the course of a burn and is an important measurement since it directly defines the motor thrust and geometry (e.g., a higher regression rate results in smaller combustion chambers) [54].…”
Section: Introductionmentioning
confidence: 99%
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