Accession Number:

ADA043408

Title:

Turbine Engine Variable Cycle Selection Program Summary.

Descriptive Note:

Final rept. Jul 73-Jan 77,

Corporate Author:

MCDONNELL AIRCRAFT CO ST LOUIS MO

Personal Author(s):

Report Date:

1977-04-01

Pagination or Media Count:

57.0

Abstract:

A systematic engineairframe evaluation procedure was developed and used to assess interactions for fixed and variable geometry engine concepts in tactical aircraft. The evaluation procedure provides a rapid and inexpensive technique for evaluations of advanced engine concepts for extensive matrices of potential aircraft maneuverability and multi-mission requirements. Author

Subject Categories:

  • Attack and Fighter Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE