cusfbamboo.circuit
Classes and functions related to thermal circuit calculations.
References
[1] - Rocket Propulsion Elements, 7th Edition
[2] - Modelling ablative and regenerative cooling systems for an ethylene/ethane/nitrous oxide liquid fuel rocket engine, Elizabeth C. Browne, https://mountainscholar.org/bitstream/handle/10217/212046/Browne_colostate_0053N_16196.pdf?sequence=1&isAllowed=y
[3] - A Simple Equation for Rapid Estimation of Rocket Nozzle Convective Heat Transfer Coefficients, Dr. R. Bartz, https://arc.aiaa.org/doi/pdf/10.2514/8.12572
[6] - Welty, Fundamentals of Momentum, Heat and Mass Transfer, Fifth Edition
Functions
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Get the heat transfer rate for a fin with an adiabatic tip (Reference [5]) |
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Get the heat flux due to nucleate boiling. |
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Get the critical heat flux due to nucleate boiling, i.e. the maximum heat transfer rate that is possible. |
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Dittus-Boelter equation for convective heat transfer coefficient. |
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Convective heat transfer coefficient for the coolant side, using Gnielinski’s correlation. |
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Sieder-Tate equation for convective heat transfer coefficient. |
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Convective heat transfer coefficient for the stable-film phase of boiling heat transfer [6]. |
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Bartz equation, using Equation (8-23) from page 312 of RPE 7th edition (Reference [1]). |
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Bartz heat transfer equation using the sigma correlation, from Reference [3]. |
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Bartz heat transfer equation using the sigma correlation, from Reference [3]. |
Classes
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Class for solving thermal circuits. |