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SAE AS681

(R) Gas Turbine Engine Performance Presentation for Computer Programs

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Organization: SAE
Publication Date: 1 June 2016
Status: active
Page Count: 26
scope:

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.

Document History

SAE AS681
June 1, 2016
(R) Gas Turbine Engine Performance Presentation for Computer Programs
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...
June 1, 2008
(R) Gas Turbine Engine Performance Presentation for Computer Programs
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...
March 1, 1999
Gas Turbine Engine Steady -State and Transient Performance Presentation for Digital Computer Programs
SCOPE: This Aerospace Standard (AS) provides the method for presentation of gas turbine engine steady-state and transient performance calculated using digital computer programs. It also provides for...
September 1, 1996
Gas Turbine Engine Steady -State and Transient Performance Presentation for Digital Computer Programs
A description is not available for this item.

References

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