Predictions by Revell's drag element model, and Hardin's total aircraft noise method where applicable, are compared with measured flyover noise spectra for different configurations of a large commercial jet transport, a business jet, a small twin-propeller aircraft, and a sailplane. These two methods had been recommended in the NASA Aircraft Noise Prediction (ANOPP) study. Predictions by a noise component method recently developed at United Technologies Research Center (UTRC) under a contract with FAA also are shown. This new method gives closest agreement with measured flyover spectra. The total aircraft noise method, which applies only for aircraft in the clean configuration, was in poor agreement with measured spectra.

  • Supplemental Notes:
    • Noise and Fluids, presented at the Winter Annual Meeting of ASME, Atlanta, Georgia, 27 November-2 December 1977.
  • Corporate Authors:

    American Society of Mechanical Engineers

    Two Park Avenue
    New York, NY  United States  10016-5990
  • Authors:
    • Fink, M R
  • Publication Date: 1977

Media Info

Subject/Index Terms

Filing Info

  • Accession Number: 00178475
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Report/Paper Numbers: Proceeding
  • Files: TRIS
  • Created Date: Aug 19 1978 12:00AM