FUTURE TRENDS IN AERO GAS TURBINE DESIGN CONVENTIONAL ENGINES

A range of possible trends in the development of high bypass ratio single stage fan engines designed for application to aircraft cruising at high subsonic Mach numbers is reviewed, placing special emphasis on trends of fuel consumption in the engine thrust sizes.

• Availability:
  • Find a library where document is available. Order URL: http://worldcat.org/issn/00019240
• Corporate Authors:

  Royal Aeronautical Society

  4 Hamilton Place
  London S1V 0BQ,   England 
• Authors:
  • Denning, R M
  • Miller, S C
  • Wright, G H
• Publication Date: 1976-8

Media Info

• Pagination: p. 343-349
• Serial:
  • Aeronautical Journal
  • Volume: 80
  • Issue Number: 788
  • Publisher: Royal Aeronautical Society
  • ISSN: 0001-9240

Subject/Index Terms

• TRT Terms: Aircraft; Ducted propellers; Engines; Fuel conservation; Fuel consumption; Gas turbines; Speed; Subsonic flow; Turbine engines
• Uncontrolled Terms: Aircraft engines
• Old TRIS Terms: Bypass engines; Ducted fan; Subsonic speed
• Subject Areas: Aviation; Energy; Planning and Forecasting; Vehicles and Equipment;

Filing Info

• Accession Number: 00152856
• Record Type: Publication
• Source Agency: Engineering Index
• Files: TRIS
• Created Date: May 31 1977 12:00AM