INVESTIGATION OF FEASIBLE NOZZLE CONFIGURATIONS FOR NOISE REDUCTION IN TURBOFAN AND TURBOJET AIRCRAFT. VOLUME II. SLOT NOZZLE CONFIGURATION

This volume contains a description of results obtained for two dimensional rectangular slot nozzles without and with straight attached flaps. Three appendices are included in this volume containing results of other research activities.

• Supplemental Notes:
  • Includes errata dated 19 May 76. See also Volume 1, AD-A024 958.
• Corporate Authors:

  University of Tennessee, Tullahoma

  Space Institute, 411 BH Goethert Parkway
  Tullahoma, TN  United States  37388-9700
• Authors:
  • Goethert, B H
  • Maus, J R
  • Dunhill, W A
  • Patterson, G T
  • Joshi, M C
• Publication Date: 1975-7

Media Info

• Pagination: 341 p.

Subject/Index Terms

• TRT Terms: Acoustics; Aerodynamic noise; Aircraft noise; Flaps (Aircraft); Fluid dynamics; Guides to the literature; Jet engines; Literature reviews; Mathematical models; Noise; Noise control; Nozzles; Shape; STOL aircraft; Turbofan engines; Turbojet engines; VTOL aircraft
• Uncontrolled Terms: Attenuation; Configuration; Models; Noise reduction; Two dimensional
• Old TRIS Terms: Aerodynamic slots; Jet engine noise; Short takeoff aircraft; Suppression
• Subject Areas: Aviation; Environment; Vehicles and Equipment;

Filing Info

• Accession Number: 00136768
• Record Type: Publication
• Source Agency: National Technical Information Service
• Report/Paper Numbers: FAA-RD-75-162-2
• Contract Numbers: DOT-FA72WA-3053
• Files: NTIS
• Created Date: Jul 13 2002 12:00AM