SAE AS 681 : 2016
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS
Hardcopy , PDF
24-08-2023
English
06-06-2016
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1. SCOPE
2. REFERENCES
3. GENERAL REQUIREMENTS
4. PROGRAMMING PRACTICES
5. PROGRAM CAPABILITIES
6. INPUT/OUTPUT
7. PROGRAM IDENTIFICATION AND TRANSMITTAL
8. PROGRAM CHECKOUT
9. NOTES
APPENDIX A
APPENDIX B
This SAE Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady-state and transient performance calculated using computer programs.
| Committee |
S-15
|
| DocumentType |
Revision
|
| Pages |
26
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
| SAE AIR 1419 : 2017 | INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES |
| SAE ARP 5571 : 2013 | GAS TURBINE ENGINE PERFORMANCE PRESENTATION AND NOMENCLATURE FOR OBJECT-ORIENTED COMPUTER PROGRAMS |
| SAE ARP7998:2023 | Shared Memory Interface for Gas Turbine Engine Performance Programs |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| SAE ARP 1420 : 2017 | GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
| SAE ARP 4148 : 2015 | GAS TURBINE ENGINE REAL TIME PERFORMANCE MODEL PRESENTATION |
| SAE ARP 1210 : 2017 | GAS TURBINE ENGINE INTERFACE TEST DATA REDUCTION COMPUTER PROGRAMS |
| SAE AIR 4548 : 2013 | REAL-TIME MODELING METHODS FOR GAS TURBINE ENGINE PERFORMANCE |
| SAE ARP 4868 : 2016 | FUNCTION-BASED API FOR GAS TURBINE ENGINE PERFORMANCE PROGRAMS |
| SAE AIR 1703 : 2012 | IN-FLIGHT THRUST DETERMINATION |
| SAE AIR 5020 : 2012 | TIME-DEPENDENT IN-FLIGHT THRUST DETERMINATION |
| SAE ARP 1257 : 1993 | GAS TURBINE ENGINE TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS |
| MIL-P-85573 Base Document:1983 | POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
| SAE AIR 5656 : 2016 | STATISTICAL STABILITY ASSESSMENT |
| SAE AS 4191 : 2015 | GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS USING FORTRAN |
| SAE AIR 5509 : 2012 | USING ENGINE TEST DATA TO MODEL ENGINE PERFORMANCE |
| SAE AIR 4065 : 2012 | PROPELLER/PROPFAN IN-FLIGHT THRUST DETERMINATION |
| SAE AS 210 : 2014(R2018) | DEFINITION OF COMMONLY USED DAY TYPES (ATMOSPHERIC AMBIENT TEMPERATURE CHARACTERISTICS VERSUS PRESSURE ALTITUDE) |
| SAE AS 6502 : 2015 | AIRCRAFT PROPULSION SYSTEM PERFORMANCE NOMENCLATURE |
| SAE AIR 5509 : 2012 | USING ENGINE TEST DATA TO MODEL ENGINE PERFORMANCE |
| SAE ARP 5571 : 2013 | GAS TURBINE ENGINE PERFORMANCE PRESENTATION AND NOMENCLATURE FOR OBJECT-ORIENTED COMPUTER PROGRAMS |
| SAE ARP 4868 : 2016 | FUNCTION-BASED API FOR GAS TURBINE ENGINE PERFORMANCE PROGRAMS |
| SAE ARP 4148 : 2015 | GAS TURBINE ENGINE REAL TIME PERFORMANCE MODEL PRESENTATION |
| SAE ARP 1210 : 2013 | GAS TURBINE ENGINE INTERFACE TEST DATA REDUCTION COMPUTER PROGRAMS |
| ISO 2533:1975 | Standard Atmosphere |
| SAE AIR 4548 : 2013 | REAL-TIME MODELING METHODS FOR GAS TURBINE ENGINE PERFORMANCE |
| MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
| SAE AS 4191 : 2015 | GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS USING FORTRAN |
| SAE ARP 1420 : 2002 | GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
| SAE AS 755 : 2014 | AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION |
| SAE TSB 003 : 1999 | RULES FOR SAE USE OF SI (METRIC) UNITS |
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