A systematic engine/airframe 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)
Turbine Engine Variable Cycle Selection Program Summary
1977
57 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Aircraft , Turbojet engines , Turbofan engines , Tactical aircraft , Fighter aircraft , Variable cycle engines , Selection , Performance(Engineering) Mission profiles) , Airframes , Propulsion systems , Sizes(Dimensions) , Cost effectiveness , Development tests , Experimental design , Matrices(Mathematics) , Mathematical analysis , Military requirements , Latin squares