24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-4.1.2

NAVIER-STOKES ANALYSIS FOR SCT LOW-SPEED HIGH-LIFT FLIGHT AND WIND TUNNEL CONFIGURATIONS
V. Brandi
CIRA - Italian Aerospace Research Center Via Maiorise, 81043, Capua (CE), Italy
Keywords: vortex flow, SCT configuration, high-lift computations, WT model installation effect

This paper deals with the flow characteristics around the Supersonic Commercial Transport wing body and 1:22 wind tunnel model at typical flyover design conditions.

view full paper

24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan Paper ICAS 2004-4.1.2

NAVIER-STOKES ANALYSIS FOR SCT LOW-SPEED HIGH-LIFT FLIGHT AND WIND TUNNEL CONFIGURATIONS

V. Brandi CIRA - Italian Aerospace Research Center Via Maiorise, 81043, Capua (CE), Italy

Keywords: vortex flow, SCT configuration, high-lift computations, WT model installation effect This paper deals with the flow characteristics around the Supersonic Commercial Transport wing body and 1:22 wind tunnel model at typical flyover design conditions.

view full paper

24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-4.1.2

V. Brandi
CIRA - Italian Aerospace Research Center Via Maiorise, 81043, Capua (CE), Italy

Keywords: vortex flow, SCT configuration, high-lift computations, WT model installation effect

This paper deals with the flow characteristics around the Supersonic Commercial Transport wing body and 1:22 wind tunnel model at typical flyover design conditions.