Accession Number : ADA268386


Title :   Structured Finite Volume Modeling of U.S. Navy Aircraft Engine Test Cells. Task 2: Turboprop Engine. Code Documentation and Listings. Volume 2


Descriptive Note : Final rept. Dec 90-Sep 92,


Corporate Author : ADAPTIVE RESEARCH CORP HUNTSVILLE AL


Personal Author(s) : Daley, P L ; Mahaffey, W A


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a268386.pdf


Report Date : Jun 1993


Pagination or Media Count : 148


Abstract : This report presents results of the numerical simulation of a U.S. Naval turboprop 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.


Descriptors :   *TURBOPROP ENGINES , TEST AND EVALUATION , INPUT , SIMULATION , COMPUTERS , FACILITIES , BOUNDARIES , FLUID DYNAMICS , TEST FACILITIES , NAVAL AIRCRAFT , COMPUTATIONAL FLUID DYNAMICS , CELLS , VOLUME , MODELS , AIRCRAFT ENGINES


Subject Categories : Aircraft
      Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE