Effect of Isogrid-Type Obstructions on Thermal Stratification in Upper-Stage Rocket Propellant Tanks
Analytical models for propellant thermal stratification are typically based on smooth wall flow correlations. However, many propellant tank walls have a mass-saving isogrid, which alters the boundary layer. This work investigates the boundary-layer behavior over walls with obstruction elements that...
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Veröffentlicht in: | Journal of spacecraft and rockets 2014-09, Vol.51 (5), p.1587-1602 |
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Format: | Artikel |
Sprache: | eng |
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