NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A Guide to Axial-Flow Turbine Off-Design Computer Program AXOD2A Users Guide for the axial flow turbine off-design computer program AXOD2 is composed in this paper. This Users Guide is supplementary to the original Users Manual of AXOD. Three notable contributions of AXOD2 to its predecessor AXOD, both in the context of the Guide or in the functionality of the code, are described and discussed in length. These are: 1) a rational representation of the mathematical principles applied, with concise descriptions of the formulas implemented in the actual coding. Their physical implications are addressed; 2) the creation and documentation of an Addendum Listing of input namelist-parameters unique to AXOD2, that differ from or are in addition to the original input-namelists given in the Manual of AXOD. Their usages are discussed; and 3) the institution of proper stoppages of the code execution, encoding termination messaging and error messages of the execution to AXOD2. These measures are to safe-guard the integrity of the code execution, such that a failure mode encountered during a case-study would not plunge the code execution into indefinite loop, or cause a blow-out of the program execution. Details on these are discussed and illustrated in this paper. Moreover, this computer program has since been reconstructed substantially. Standard FORTRAN Langue was instituted, and the code was formatted in Double Precision (REAL*8). As the result, the code is now suited for use in a local Desktop Computer Environment, is perfectly portable to any Operating System, and can be executed by any FORTRAN compiler equivalent to a FORTRAN 9095 compiler. AXOD2 will be available through NASA Glenn Research Center (GRC) Software Repository.
Document ID
20140010362
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Chen, Shu-Cheng S.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
July 31, 2014
Publication Date
June 1, 2014
Subject Category
Computer Programming And Software
Aircraft Propulsion And Power
Report/Patent Number
E-18884
NASA/TM-2014-218301
GRC-E-DAA-TN12340
Report Number: NASA/TM-2014-218301
Report Number: GRC-E-DAA-TN12340
Report Number: E-18884
Funding Number(s)
WBS: WBS 794072.02.03.05.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Gas Turbine Engines
Axial Flow Turbines
Design Analysis
No Preview Available