SAE AS681K
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Gas Turbine Engine Performance Presentation for Computer Programs
Hardcopy , PDF
English
06-06-2016
24-08-2023
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Superseded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.
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