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GAS TURBINE ENGINE STEADY-STATE AND TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS
- Aerospace Standard
- AS681G
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Topic
Data Sets - Support Documents
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| TABLE 1 | Power Code Assignments | |
| TABLE 2 | Rating Code Assignments | |
| TABLE 3 | SERAM Assignments | |
| TABLE 4 | SECALC Assignment | |
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| TABLE 5 | First Digit Numerical Status Indicator Assignments | |
| TABLE 6 | Second Digit Numerical Status Indicator Assignments | |
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Issuing Committee
S-15 Gas Turbine Perf Simulation Nomenclature and Interfaces
Welcome to the SAE S-15, Engine Performance Simulation Nomenclature and Interfaces Forum.
Scope: The committee provides recommendations relative to the information contained in mathematical models of aerospace engines and their derivatives and to the coordination of the interfaces between models suppliers and their users. For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright, and Membership" link in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expresed or information posted in this forum. All information posted becomes the property of SAEReference
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