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:
  • 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

Filing Info

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