Standard

SAE AS681F

Withdrawn

Existing or new amendments and versions must be purchased separately.

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Abstract

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.

Products specifications

  • Standard from SAE International
  • Published:
  • Withdrawn:
  • Document type: IS
  • Pages
  • Publisher: SAE International
  • Distributor: SAE International

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