In today's highly competitive and economically driven commercial aviation market, the trend is to make aircraft systems simpler and to shorten their design cycle which reduces recurring, non-recurring and operating costs. One such system is the high-lift system. A methodology has been developed which merges aerodynamic data with kinematic analysis of the trailing-edge flap mechanism with minimum mechanism definition required. This methodology provides quick and accurate aerodynamic performance prediction for a given flap deployment mechanism early on in the high-lift system preliminary design stage. Sample analysis results for four different deployment mechanisms are presented as well as descriptions of the aerodynamic and mechanism data required for evaluation. Extensions to interactive design capabilities are also discussed.
Aero-Mechanical Design Methodology for Subsonic Civil Transport High-Lift Systems
2000-06-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aero-Mechanical Design Methodology for Subsonic Civil Transport High-Lift Systems
British Library Conference Proceedings | 2000
|High- Lift Design Methodology For Subsonic Civil Transport Aircraft
British Library Conference Proceedings | 2000
|