ARP876 is intended to provide specific recommended procedures for the prediction of gas turbine jet exhaust system noise sources. Procedures are issued as separate sections, to allow for future updating as additional methods, consistent with state-of-the-art, become available. Revision F corrects an error in Equation 9 for the single stream shock-associated noise prediction method, and corrects an error in Table 14 for the mixed component Z4 term of the subsonic coaxial jet mixing noise prediction method.
Gas Turbine Jet Exhaust Noise Prediction
05.01.2021
Aufsatz (Konferenz)
Englisch
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