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SAE AS681 Rev L

Gas Turbine Engine Performance Presentation for Computer Programs
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SAE AS681 Rev L

Gas Turbine Engine Performance Presentation for Computer Programs

PUBLISH DATE 2023
PAGES 27
SAE AS681 Rev L
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, but not limited to, the following program types: data reduction, steady-state, transient, preliminary design, study, specification, status, and parametric programs.
SDO SAE: SAE International
Document Number AS681
Publication Date Aug. 21, 2023
Language en - English
Page Count 27
Revision Level L
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