title: Similarity spectra analysis of high-performance jet aircraft noise.
abstract: Noise measured in the vicinity of an F-22A Raptor has been compared to similarity spectra found previously to represent mixing noise from large-scale and fine-scale turbulent structures in laboratory-scale jet plumes. Comparisons have been made for three engine conditions using ground-based sideline microphones, which covered a large angular aperture. Even though the nozzle geometry is complex and the jet is nonideally expanded, the similarity spectra do agree with large portions of the measured spectra. Toward the sideline, the fine-scale similarity spectrum is used, while the large-scale similarity spectrum provides a good fit to the area of maximum radiation. Combinations of the two similarity spectra are shown to match the data in between those regions. Surprisingly, a combination of the two is also shown to match the data at the farthest aft angle. However, at high frequencies the degree of congruity between the similarity and the measured spectra changes with engine condition and angle. At the higher engine conditions, there is a systematically shallower measured high-frequency slope, with the largest discrepancy occurring in the regions of maximum radiation.
authors.affiliation: Department of Physics and Astronomy, N283 ESC, Brigham Young University, Provo, Utah 84602, USA. tbn@byu.edu
authors.forename: Tracianne B
authors.initials: TB
authors.lastname: Neilsen
authors.forename: Kent L
authors.initials: KL
authors.lastname: Gee
authors.forename: Alan T
authors.initials: AT
authors.lastname: Wall
authors.forename: Michael M
authors.initials: MM
authors.lastname: James
mesh_terms: D000162:Acoustics / Q000295:instrumentation; D000401:Aircraft; D008962:Models, Theoretical; D009624:Noise, Transportation; D012815:Signal Processing, Computer-Assisted; D013018:Sound Spectrography; D014159:Transducers