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Document type:
Semesterarbeit 
Type detailled:
Theoretisch 
Author(s):
Illenberger, Gerrit Markus 
E-mail address:
gerrit.illenberger@tum.de 
Title:
Numerical Investigations on the Static Aeroelasticity of a Sailplane with a Morphing Forward Wing Section 
Abstract:
An alternative structural concept in the wing design of sailplanes is the combination of a morphing forward wing section with a conventional trailing edge flap. Since the load-bearing wing cross section is reduced by a droop nose, the torsional stiffness of the structure decreases. This leads, under aerodynamic load, to undesirable twisting, which in turn deteriorates the aerodynamic efficiency of the wing. The present thesis deals with the investigation of a structural preliminary design with r...    »
 
Keywords:
Aeroelasticity, Aeroelastic Tailoring, DLM, FEM, Morphing Wing 
Subject:
MAS Maschinenbau 
Advisor:
Hornung, Mirko; Sturm, Fabian 
Year:
2019 
University:
Technical University of Munich 
Faculty:
Fakultät für Maschinenwesen 
TUM Institution:
Institute of Aircraft Design