Prediction of the ullage gas thermal stratification in a NASP vehicle propellant tank experimental simulation using FLOW-3D
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[1] C. W. Hirt,et al. Volume of fluid (VOF) method for the dynamics of free boundaries , 1981 .
[2] J. Navickas,et al. Modeling of solid-liquid circulation in the National Aerospace Plane's slush hydrogen tanks , 1988 .
[3] Ned P. Hannum. Technology issues associated with fueling the national aerospace plane with slush hydrogen , 1988 .
[4] G. P. Richter,et al. Slush Hydrogen (SLH2) Technology Development for Application to the National Aerospace Plane (NASP) , 1990 .
[5] F. Harlow,et al. Numerical Calculation of Time‐Dependent Viscous Incompressible Flow of Fluid with Free Surface , 1965 .
[6] C. W. Hirt,et al. Zero-gravity slosh analysis , 1985 .
[7] A. A. Amsden,et al. A numerical fluid dynamics calculation method for all flow speeds , 1971 .
[8] J. Navickas,et al. Prediction of a liquid tank thermal stratification by a finite difference computing method , 1988 .
[9] J. E. Maloy,et al. Gaseous hydrogen requirements for the discharge of liquid hydrogen from a 1.52 meter /5 ft/ diameter spherical tank , 1970 .
[10] Richard L. DeWitt,et al. Gaseous-Hydrogen Pressurant Requirements for the Discharge of Liquid Hydrogen from a 3.96 Meter /13 ft/ Diameter Spherical Tank , 1969 .
[11] C. W. Hirt,et al. Numerical simulation of propellant sloshing for spacecraft , 1984 .
[12] P. A. Masters. Computer programs for pressurization (RAMP) and pressurized expulsion from a cryogenic liquid propellant tank , 1974 .
[13] R. Hussey,et al. Spin‐up from rest in a cylinder , 1977 .