Aircraft structure design is a complex industrial process that requires multidisciplinary
analyzes and considerations in fields as diverse as aerodynamics, structure, materials and …

This article presents an approach to set turbulent wedges and transition trip**s in local
correlation-based intermittency transport transition models. Turbulent wedges are created by …

The unsteady boundary layer behavior of a supercritical laminar airfoil model, which
undergoes limit cycle oscillations in pitch, is investigated by the application of hot-film …

Laminar flow technologies have taken a leading role concerning the pioneering
technologies for the ecofriendly aircraft of tomorrow. Leading to drag reduction, it is the aim …

MECHANISMS OF TRANSONIC SINGLE DEGREE OF FREEDOM FLUTTER OF A LAMINAR
AIRFOIL Page 1 International Forum on Aeroelasticity and Structural Dynamics IFASD 2019 …

Promising results are obtained by NASA with the CRM-NLF laminar wing at design
conditions. The work presented seeks to develop an understanding of the transition …

The transition from laminar to turbulent boundary layer has been largely investigated in the
literature on the experimental side as well as on the numerical side but the processes …

Within the European Clean Sky 2 Airframe ITD/NACOR project, a 2D airfoil laminar model
was designed, manufactured, highly instrumented and tested in the Onera S2MA transonic …

Subject of the present work is the development of nonlinear model-order reduction methods
based on recurrent neuro-fuzzy approaches to efficiently predict motion-induced unsteady …

High fidelity aeroelastic simulations of laminar wings require an accurate prediction of the
aerodynamic forces taking into account non-linear phenomena due to the laminar-turbulent …