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Označení normy: SAE AIR5826B
Datum vydání normy: 1.3.2017
Kód zboží: NS-678206
Země: Americká technická norma
Kategorie: Technické normy SAE
This document provides a review of published methods that have been used to provide estimates of the levels of distortion and/or the concomitant loss of stability pressure ratio that can occur when the recommended full complement of aerodynamic interface plane high-response instrumentation is not used when obtaining inlet data. The methods have been categorized based on the underlying mathematical representation of the aerophysics. Further, the use of maximum value statistics, which has been used to further improve the results where short-duration time records have been employed, is discussed.
SUBJECT TAXONOMY: Simulation and modeling, Engines, Gas turbines
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
Stabilized: Mar 2017
Poslední aktualizace: 09.09.2024 (Počet položek: 2 346 212)
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