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SAE AS681K

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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

Available format(s)

Hardcopy , PDF

Superseded date

24-08-2023

Superseded by

SAE AS681L

Language(s)

English

Published date

06-06-2016

€134.60
Excluding VAT

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Superseded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
MIL BULL 343 : A DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
SAE ARP1420C Gas Turbine Engine Inlet Flow Distortion Guidelines
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
SAE AIR5020A 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 AIR5656A Statistical Stability Assessment
SAE AS 4191 : 2015 GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS USING FORTRAN
SAE AIR5509 Using Engine Test Data to Model Engine Performance
SAE AIR4065A 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 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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