Numerical Prediction of Transient Axial Thrust and Internal Flows in a Rocket Engine Turbopump The program employs a finite volume formulation of mass, momentum, and energy conservation equations in conjunction with the thermodynamic equation of state of real fluids. Predicted results were then compared...
The differential equation of motion for systems with mass ejection (rocket equation) or mass accretion is also derived.John T. KatsikadelisSchool of Civil EngineeringNational Technical University of AthensActa MechanicaKatsikadelis , J.T. : Derivation of Newton's law of motion using Galileo's ...
The derived equation provides a mathematical solution to determine the heat transfer rate for a system of cryogenic pipe insulated with multiple layers. 展开 关键词: Cryogenic Liquid nitrogen Pipe flow Thermal insulation system Three-dimensional heat conductivity ...
Plasmas (high-temperature, highly charged gases) arise in important applications like rocket exhaust and space-vehicle re-entry. Microscopically, a plasma consists of particles grazing each other, and the goal has been to arrive at the linear Landau equation (which describes it macroscopically) via...