Standard

SAE AS681F

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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.

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  • Standard da SAE International
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  • Tipo di documento: IS
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  • Publisher SAE International
  • Distributor SAE International

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