The effects of fuel economy structures and of noise abatement requirements on aircraft engine design are considered. Prop fan and geared fan engines, heat exchanger engines, variable cycle engines, variable pitch turbofans, boundary layer propulsion systems and laminar flow control technology are all reviewed in brief.

  • Corporate Authors:

    Shell Oil Company

    1 Shell Plaza, P.O. Box 2463
    Houston, TX  United States  77001
  • Authors:
    • Denning, R M
    • Miller, S C
    • Wright, G
  • Publication Date: 1976

Media Info

Subject/Index Terms

Filing Info

  • Accession Number: 00172822
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Files: TRIS
  • Created Date: Jun 28 1978 12:00AM