AIRCRAFT CONFIGURATION NOISE REDUCTION. VOLUME II. COMPUTER PROGRAM USER'S GUIDE AND OTHER APPENDICES

This report is volume 2 of the series and was prepared jointly by the Noise Technology Staff of the Boeing Commercial Airplane Company and the Noise Systems Group of Boeing Computer Services, Inc. This volume contains: The user's guide for the computer software of the Aircraft Configuration Noise Reduction study; A preliminary test plan for assessing forward velocity effects on wing and fuselage shielding; and Various curves, derivations, and background theory in support of material presented in volume 1.

• Supplemental Notes:
  • See also Volume 3, AD-A030 657.
• Corporate Authors:

  Boeing Company

  P.O. Box 3707, Commercial Airplane Group
  Seattle, WA  United States  98124
• Authors:
  • Dunn, D G
  • Cecil, D J
  • Butzel, L M
  • Campbell, J M
  • Lu, H Y
• Publication Date: 1976-6

Media Info

• Pagination: 140 p.

Subject/Index Terms

• TRT Terms: Aircraft noise; Computer programs; Diffraction; Fuselages; Interfaces; Jet engines; Manuals; Needs assessment; Noise; Noise control; Shape; Subroutines; Velocity; Wings (Aircraft)
• Uncontrolled Terms: Configuration; Noise reduction; User needs
• Old TRIS Terms: Jet engine noise
• Subject Areas: Aviation; Environment;

Filing Info

• Accession Number: 00146020
• Record Type: Publication
• Source Agency: National Technical Information Service
• Report/Paper Numbers: FAA-RD-76-76-2 Final Rpt., D6-42849-2
• Contract Numbers: DOT-FA74WA-3497
• Files: NTIS, TRIS
• Created Date: Jan 16 1977 12:00AM