Structured Finite Volume Modeling of U.S. Navy Aircraft Engine Test Cells. Task 1: Turboshaft Engine. Final Report Volume 1.

Abstract

This report presents results of the numerical simulation of a U.S. Naval turboshaft 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 turboshaft test cells.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1993
Accession Number
ADA268176

Entities

People

  • P..l. Daley
  • W.a. Mahaffey

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircraft Engines
  • Aircrafts
  • Boundaries
  • Civil Engineering
  • Computational Fluid Dynamics
  • Energy Systems
  • Engines
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Mechanics
  • Simulations
  • Temperature Gradients
  • Test Facilities
  • Three Dimensional
  • Turboshaft Engines
  • Two Dimensional

Readers

  • Business Analytics
  • Computational Fluid Dynamics (CFD)
  • Petroleum Engineering