A Prediction Procedure for Propeller Aircraft Flyover Noise Based on Empirical Data 810604
Forty-eight different flyover noise certification tests are analyzed using multiple linear regression methods. A prediction model is presented based on this analysis, and the results compared with the test data and two other Prediction methods. The aircraft analyzed include 30 single engine aircraft, 16 twin engine piston aircraft, and two twin engine turboprops. The importance of helical tip Mach number is verified and the relationship of several other aircraft, engine, and propeller parameters is developed. The model shows good agreement with the test data and is at least as accurate as the other prediction methods. It has the advantage of being somewhat easier to use since it is in the form of a single equation.
Citation: Smith, M., "A Prediction Procedure for Propeller Aircraft Flyover Noise Based on Empirical Data," SAE Technical Paper 810604, 1981, https://doi.org/10.4271/810604. Download Citation
Author(s):
Michael H. Smith
Pages: 14
Event:
Business Aircraft Meeting and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 1981Transactions-V90-A
Related Topics:
Aircraft
Pistons
SAE MOBILUS
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