2008
DOI: 10.1002/fld.1779
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Surrogate model‐based strategy for cryogenic cavitation model validation and sensitivity evaluation

Abstract: Cryogenic cavitation experiences phase change in an environment where the vapor pressure is temperature dependent. The cavitation dynamics have critical implications on the performance and safety of liquid rocket engines, but there is no established method to estimate the actual loads due to cavitation on the inducer blades. To help develop such a computational capability, we conduct a systematic investigation of a transport-based, homogeneous cryogenic cavitation model for code validation and model improvemen… Show more

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Cited by 46 publications
(55 citation statements)
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“…Equation 3 clearly shows the temperature dependency of cavitation, and the local temperature drop in cryogenic cavitation will produce a noticeable rise for the local cavitation number σ and hence suppress the cavitation intensity compared with that under isothermal assumption [9]. The detail impact for the thermal-sensible material properties to cavitation model will be introduced later.…”
Section: Cavitationmentioning
confidence: 97%
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“…Equation 3 clearly shows the temperature dependency of cavitation, and the local temperature drop in cryogenic cavitation will produce a noticeable rise for the local cavitation number σ and hence suppress the cavitation intensity compared with that under isothermal assumption [9]. The detail impact for the thermal-sensible material properties to cavitation model will be introduced later.…”
Section: Cavitationmentioning
confidence: 97%
“…For cryogenic cavitation, the actual local cavitation number σ needs to be corrected according to the local temperature: σ = (P ∞ − P v (T ))/0.5ρ l U 2 ∞ . Utturkar et al [1] and Goel et al [9] use the first order approximation as follows…”
Section: Cavitationmentioning
confidence: 99%
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