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GAS TURBINE ENGINE STEADY-STATE AND TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS
- Aerospace Standard
Published September 01, 1996 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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.
Data Sets - Support Documents
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|TABLE 1||Power Code Assignments|
|TABLE 2||Rating Code Assignments|
|TABLE 3||SERAM Assignments|
|TABLE 4||SECALC Assignment|
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|TABLE 5||First Digit Numerical Status Indicator Assignments|
|TABLE 6||Second Digit Numerical Status Indicator Assignments|
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S-15 Gas Turbine Perf Simulation Nomenclature and Interfaces
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