SACCON Static Wind Tunnel Tests at DNW-NWB and 14´x22´ NASA LaRC

Abstract

Static force and pressure measurement results obtained from test campaigns in two different wind tunnels are presented. The model investigated was the generic UCAV configuration SACCON. Model design, build as well as three wind tunnel entries have been performed within the NATO/RTO AVT-161 Task Group “Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles”. The model has undergone static as well as dynamic tests as an international co-operation; the tests have been accompanied by corresponding numerical investigations. This paper covers the static part of the wind tunnel experiments.