Multidimensional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis
“Multidimensional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis” by Ten-See Wang is a technical study published by BiblioLife in August 2013. This 24-page work presents a unified computational analysis aimed at determining design parameters such as axial thrust and heat fluxes for regeneratively cooled liquid rocket engine nozzles, utilizing advanced computational methodologies.
Readers will find a detailed examination of the computational strategies employed, which include a multidimensional, finite-volume approach that accounts for turbulent, chemically reacting, and radiating conditions. The study systematically investigates various factors, including wall boundary conditions and combustion chemistry, to assess their impact on performance metrics. This edition provides insights into the computational framework and methodologies that yield results consistent with existing data, making it a resource for those interested in the technical aspects of rocket engine design and performance analysis.
Official synopsis Publisher
The objective of this study is to conduct a unified computational analysis for computing design parameters such as axial thrust, convective and radiative wall heat fluxes for regeneratively cooled liquid rocket engine nozzles, so as to develop a computational strategy for computing those parameters through parametric investigations. The computational methodology is based on a multidimensional, finite-volume, turbulent, chemically reacting, radiating, unstructured-grid, and pressure-based formulation, with grid refinement capabilities. Systematic parametric studies on effects of wall boundary conditions, combustion chemistry, radiation coupling, computational cell shape, and grid refinement were performed and assessed. Under the computational framework of this study, it is found that the computed axial thrust performance, flow features, and wall heat fluxes compared well with those of available data and calculations, using a strategy of structured-grid dominated mesh, finite-rate chemistry, and cooled wall boundary condition.
FAQ
What is “Multidimensional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis” about?
Who is the author of “Multidimensional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis”?
When was “Multidimensional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis” published?
What is the ISBN for “Multidimensional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis”?
What are the book details (language, pages, edition)?
