Liquid hydrogen (LH2) is the highest specific impulse rocket fuel commonly available. However, launch systems using LH2 are informed by flow boiling heat transfer and pressure drop correlations, the most recent of which has up to 50% root-mean-squared error. This error is exacerbated because no previous experiments have optically verified cryogenic multiphase flow regimes concurrent with heat transfer measurements in pipes with diameter larger than 14.1 mm. To address this gap, this thesis presents the development of a two-phase hydrogen flow cell that can address uncertainty in existing models by providing temperature, velocity, and pressure drop data while visually identifying flow regimes. Results using liquid nitrogen are provided with comparison to recent flow boiling correlations for heat transfer coefficient, pressure, quality, and velocity. Recommendations are made for correlation modification with demonstrated predictive improvement.
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Title
HEAT FLUX IN LOW MASS FLUX HORIZONTAL CRYOGENIC FLOW
Creators
Ian Arthur Wells
Contributors
Jacob W Leachman (Chair)
Konstantin Matveev (Committee Member)
John McCloy (Committee Member)
Awarding Institution
Washington State University
Academic Unit
School of Mechanical and Materials Engineering
Theses and Dissertations
Master of Science (MS), Washington State University
Number of pages
230
Identifiers
99901297674801842
Language
English
Resource Type
Thesis
WellsIan-MastersThesis-Final-Final
Dataset to accompany: Heat flux in low mass flux horizontal cryogenic flow