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.
This document has been revised to align with the creation of and/or updates to standard documents AS6502, AS755, AS4191, and AS210. Also, supplier/customer model delivery points of discussion were added to improve the efficiency of model delivery. An S-15 document family tree was added to illustrate the relationships of the documents referenced within this document. In addition, other minor changes were also made for clarification purposes.