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SAE AS681

Revision K, June 1, 2016

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(R) Gas Turbine Engine Performance Presentation for Computer Programs



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Product Details:

  • Revision: Revision K, June 1, 2016
  • Published Date: May 2016
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 26
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

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.

AIA/NAS Aerospace Standards