4:40 PM - 5:00 PM
[3-08-3-01] Steady 1D Non-Adiabatic Viscous Flow Model for Design and Assessment of Nuclear Fuel Element Coolant Channels with Variable Geometry
Keywords:Gasdynamics, Nuclear Thermal Propulsion, Non-Adiabatic Viscous Flow, Nozzle, Rao Method, One-dimensional Flow, Variable Geometry Coolant Channels
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