DEVELOPMENT OF CRITERIA FOR THE DESIGN OF A LOW NOISE LEVEL GENERAL AVIATION PROPELLER

The theoretical and experimental investigation of general aviation propellers is considered. The objective is to improve noise generation characteristics without loss of performance. (Author)

• Corporate Authors:

  University of Illinois, Urbana-Champaign

  Department of Aeronautical and Astronautical Engineering
  Urbana, IL  United States  61801
• Authors:
  • Ormsbee, A I
• Publication Date: 1976-8

Media Info

• Pagination: 102 p.

Subject/Index Terms

• TRT Terms: Aircraft; Aircraft noise; Analysis; Cavitation noise; Design; General aviation aircraft; Noise; Noise control; Propellers; Sound level; Vehicle performance
• Uncontrolled Terms: Design criteria; Noise reduction
• Old TRIS Terms: Aircraft performance; Noise sound
• Subject Areas: Aviation; Design; Environment; Vehicles and Equipment;

Filing Info

• Accession Number: 00146738
• Record Type: Publication
• Source Agency: National Technical Information Service
• Report/Paper Numbers: NASA-CR-147979 Status Rpt
• Contract Numbers: NGR-14-005-194
• Files: TRIS
• Created Date: Feb 16 1977 12:00AM