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Gas Turbine Engine Performance Presentation for Computer Programs Using Fortran
- Aerospace Standard
Published May 13, 2021 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Standard (AS) provides a method for gas turbine engine performance computer programs to be written using Fortran COMMON blocks. If a “function-call application program interface” (API) is to be used, then ARP4868 and ARP5571 are recommended as alternatives to that described in this document.
When it is agreed between the program user and supplier that a particular program shall be supplied in Fortran, this document shall be used in conjunction with AS681 for steady-state and transient programs.
This document also describes how to take advantage of the Fortran CHARACTER storage to extend the information interface between the calling program and the engine subroutine.
This document has been revised to align with the creation of standard document AS6502 and updates to standard document AS681. Other minor changes were also made for clarification purposes
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|SAE ITC E&A Standard||AS46732 Thrust Wire - Nut Union, Male (Steel)|
|Aerospace Material Specification||Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 47.5ni 22cr 1.5co 9.0mo 0.60w 18.5fe, Solution Heat Treated|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Table 1||Inlet mode selection|
|Table 2||Inlet ram pressure recovery options (SERAM)|
|Table 3||ERAMX arguments|
|Table 4||Minimum input list - FIXIN|
|Table 5||Minimum output list - FIXOUT|
|Unnamed Dataset 8|
|Unnamed Dataset 9|
|Table 6||First digit numerical status indicator assignments|
|Table 7||Second digit numerical status indicator assignments|
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