Description / Abstract:
This Aerospace Recommended Practice provides a method for the
presentation of gas turbine engine
transient performance as calculated by means of digital computer
programs and is compatible with
AS681, Gas Turbine Engine Steady-State Performance Presentation for
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.
Note: Applicable reference documents are listed in Section 10.