SAE AS681K
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
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.
DocumentType |
Standard
|
Pages |
26
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
This SAE Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady-state and transient performance calculated using computer programs. It also provides for the presentation of parametric gas turbine data including performance, weight, and dimensions computed by computer programs.This standard is intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier. This standard is applicable to, but not limited to the following program types: data reduction, steady-state, transient, preliminary design, study, specification, status, and parametric programs.
JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
SAE AIR1419C | Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines |
SAE ARP5571B | Gas Turbine Engine Performance Presentation and Nomenclature For Object-Oriented Computer Programs |
SAE ARP7998 | Shared Memory Interface for Gas Turbine Engine Performance Programs |
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SAE ARP 4148 : 2015 | GAS TURBINE ENGINE REAL TIME PERFORMANCE MODEL PRESENTATION |
SAE ARP1210E | Gas Turbine Engine Interface Test Data Reduction Computer Programs |
SAE AIR4548A | Real-Time Modeling Methods for Gas Turbine Engine Performance |
SAE ARP4868C | Function-Based API for Gas Turbine Engine Performance Programs |
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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 AIR5509 | Using Engine Test Data to Model Engine Performance |
SAE ARP5571B | Gas Turbine Engine Performance Presentation and Nomenclature For Object-Oriented Computer Programs |
SAE ARP4868C | Function-Based API for Gas Turbine Engine Performance Programs |
SAE ARP 4148 : 2015 | GAS TURBINE ENGINE REAL TIME PERFORMANCE MODEL PRESENTATION |
SAE ARP1210D | Gas Turbine Engine Interface Test Data Reduction Computer Programs |
ISO 2533:1975 | Standard Atmosphere |
SAE AIR4548A | 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 AS755E | Aircraft Propulsion System Performance Station Designation and Nomenclature |
SAE TSB003_199905 | Rules for SAE Use of SI (Metric) Units |
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