01.1 - Aircraft Design and Integrated System (Basics and Theory)
PERFORMANCE AND ECONOMIC ASSESSMENT OF A WING-INTEGRATED HYBRID LAMINAR FLOW CONTROL SYSTEM
B.M.H.J. Fröhler¹, A.A. Pohya¹, J. Häßy¹, T. Kilian¹, A.H. Bismark¹, M. Radestock, Germany; D. Cruz Palacios, Aernnova Aerospace, Spain; ¹German Aerospace Center (DLR), Germany
This study demonstrates the integration of a HFLC system into a wing in an industrial context. The goal is to evaluate the HLFC system objectively by comparing to a non-HLFC aircraft. The assessment covers a mission performance estimation and a life cycle simulation with three scenarios to determine fuel and cost savings.