Abstract
A preliminary analysis of F/A-18E Super Hornet static engine run-up noise measurements that shows evidence of nonlinear propagation effects was described. Evidence of nonlinear propagation was demonstrated by a comparison of measured spectra with free-field linear predictions and by calculation of a nonlinear indicator. Analysis of the F/A-18E static engine run-up measurements indicated that the noise is non-Gaussian and the propagation nonlinear at afterburner and military thrust conditions. The study has demonstrated that additional and perhaps more extensive investigations in this area are merited.
Original language | English (US) |
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Pages (from-to) | 1398-1401 |
Number of pages | 4 |
Journal | AIAA journal |
Volume | 43 |
Issue number | 6 |
DOIs | |
State | Published - Jun 2005 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering