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SAE ARP1257

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SAE ARP1257 Revision A, October 20, 1989 Gas Turbine Engine Transient Performance Presentation for Digital Computer Programs
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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.