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Numerical Study of High Temperature and High Velocity Gaseous Hydrogen Flow in a Cooling Channel of a Nuclear Thermal Rocket Core
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Two mathematical models (a onedimensional (1D) and a twodimensional (2D)) were adopted to study, numerically, the thermalhydrodynamic characteristics of flow inside the cooling channels of a nuclear thermal rocket (NTR) ...
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