Supersonic commercial transport aircraft (SCT) are known for their short travel times and also for their low-speed noise. This paper focuses on the aerodynamic design of low-drag SCT high-lift systems contributing significant low-speed noise reductions by enabling steeper climbing. The high-lift system design - relying on separated flow- and validation work at DLR will be reported.
Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft
2006
8 Seiten
Aufsatz (Konferenz)
Englisch
EPISTLE: High lift system design for low-noise applied to a supersonic aircraft
Online Contents | 2006
|Noise Characteristics of Aircraft High Lift Systems
AIAA | 2003
|Noise characteristics of aircraft high lift systems
Tema Archiv | 2003
|AIAA | 1963
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