Structured Finite Volume Modeling of U.S. Navy Aircraft Engine Test Cells Task 2:Turboprop Engine Vol 1

摘要

This report presents results of the numerical simulation of a U.S. Navalturboprop test cell facility. The ultimate purpose of this simulation was to provide the Navy with a numerical model to be used for the evaluation of the aerothermal performance of test cells. This simulation was performed using the structured finite volume (SFV) computer code. A description of the physical model, mathematical details, boundary conditions, and results of the study are presented and covered in Volume 1. Volume 2, Code Documentation and Listings, provides a copy of the input files developed for the modeling of turboprop test cells.... Computational fluid dynamics, Test cells, Aviation test facilities.