SAE AS681G PDF
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GAS TURBINE ENGINE STEADY-STATE AND TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS
Description
This Aerospace Standard (AS) provides a method for the presentation of gas turbine engine steady-state and/or transient performance as calculated by means of digital computer programs. It also provides a method for the presentation of gas turbine parametric performance, weight and dimensions by means of digital computer programs.
It is intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier.
History
| AS681L | 2023-08-21 | Latest | Revised |
| AS681K | 2016-06-06 | Historical | Revised |
| AS681J | 2008-06-12 | Historical | Revised |
| AS681H | 1999-03-01 | Historical | Revised |
| AS681G | 1996-09-01 | Historical | Revised |
| AS681F | 1991-10-28 | Historical | Revised |
| AS681E | 1982-10-01 | Historical | Revised |
| AS681D | 1982-10-01 | Historical | Revised |
| AS681C | 1974-04-15 | Historical | Revised |
| ISSUING COMMITTEE | S-15 Gas Turbine Perf Simulation Nomenclature and Interfaces |
|---|---|
| DATE | 1996-09-01 |
| DOI | |
| ISCURRENT | |
| PAGE | 33 |
| PUBLISHER | SAE International |
| REVISED | REVISED |
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