01.1 - Aircraft Design and Integrated System (Basics and Theory)
AERODYNAMIC DESIGN AND ANALYSIS OF HLFC WINGS WITHIN THE EUROPEAN PROJECT HLFC-WIN
T. Streit¹, M. Kruse¹, T. Kilian¹, J. v. Geyr, DLRK, Germany; I. Petropoulos, ONERA, France; ¹DLR, Germany
Results for the numerical aerodynamic design and analysis of a long range, large passenger aircraft equipped with a Hybrid Laminar Flow Control (HLFC) system are presented. In addition, extensions of the numerical methods used to predict the transition line position in the case of suction are described.