An advanced version of the propeller airplane interior noise (PAIN) model [L. D. Pope, J. Acoust. Soc. Am. 88, 2755–2765 (1990)] can generate a prediction of the variation of the cabin cross-section average sound-pressure level of a transmitted propeller tone. The prediction can then be averaged along the length of the cabin to obtain the cabin volume average sound-pressure level, the latter being the only quantity that the original version of the PAIN model [L. D. Pope, E. G. Wilby, and J. F. Wilby, J. Sound Vib. 118, 449–467 (1987); L. D. Pope, C. M. Willis, and W. H. Mayes, ibid. 118, 469–493 (1987)] calculated. Of considerable interest is a comparison of the two volume average predictions because the advanced and original models are based on fundamentally different types of analyses. The original model predicts the response of each individual acoustic mode caused by each structural mode, leading to the average sound-pressure level within the cabin volume. The advanced version predicts the response of the entire complement of acoustic modes having a common cross mode index for each exciting structural mode. The average sound level in cabin cross section is obtained, as well as the cabin volume average. Close agreement in the two predictions of the average cabin level yields a higher level of confidence in both prediction results, compared to the independent predictions, particularly in circumstances where comparisons with flight measurements are minimal or nonexistent. Recently, during parametric studies, modifications were made to the advanced model to obtain better agreement between the two average predictions. This paper presents the revisions (upgrades) that were found to be necessary for consistency in the cabin trim absorption models. A demonstration is given of the present prediction capability through example benchmark calculations for two representative airplanes. Finally, the general usefulness of benchmark calculations and necessity of validation efforts in the development of interior noise prediction software are discussed.
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