Aircraft Design, Testing and Performance

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Buckling of fuselages until collapse


Presently the development of fast simulation tools for the post buckling behavior of fuselages is based on panel level, typically comprising a segment of 2-3 frames and 5-10 stringers.
http://www.dlr.de/fa/en/desktopdefault.aspx/tabid-4586/7649_read-11519/
Related Topics: Aircraft Stability and Control Numerical Analysis Aircraft Design, Testing and Performance

Aeroelastic Stability and System Response


The major part of the activities of the group “Aeroelastic Stability and System Response” is concerned with the aeroelasticity of civil and military transport aircraft. However, small business aircraf...
http://www.dlr.de/ae/en/desktopdefault.aspx/tabid-4118/6525_read-9277/
Related Topics: Aircraft Stability and Control Structural Mechanics Aircraft Design, Testing and Performance Aerodynamic

ALCAS


Das von der EU geförderte Forschungsprojekt ALCAS (Advanced Low Cost Aircraft Structures) hat die Erforschung von Design- und Herstellungskonzepten zur Kostenreduktion von Flugzeugkomponenten während ...
http://www.dlr.de/bk/en/desktopdefault.aspx/tabid-4523/7399_read-10108/
Related Topics: Aircraft Design, Testing and Performance

Journal Publication


An article publication on the topic of system analysis of aircraft with natural laminar flow and forward swept wings has been successfully published in the CEAS Aeronautical Journal.
http://www.dlr.de/lk/en/desktopdefault.aspx/tabid-4447/7274_read-46602/
Related Topics: Fluid Mechanics and Thermodynamics Aircraft Design, Testing and Performance

CFRP Fuselage


CFRP Fuselage comprises concepts for future aircraft fuselages, mainly based on carbon fibre composites.
http://www.dlr.de/fa/en/desktopdefault.aspx/tabid-1312/2029_read-25076/
Related Topics: Aircraft Design, Testing and Performance

DG 300


The performance of the DG 300-17 has been accurately measured, so it can be used as a calibration standard for measuring the speed polar of gliders.
http://www.dlr.de/fb/en/desktopdefault.aspx/tabid-3707/5786_read-8388/
Related Topics: Aircraft Design, Testing and Performance

Loads Analysis and Aeroelastic Design


The Loads Analysis and Aeroelastic Design Department is concerned with questions that arise in the context of aircraft design with regard to aeroelastic properties or aeroelastic requirements. In addi...
http://www.dlr.de/ae/en/desktopdefault.aspx/tabid-8350/6541_read-9334/
Related Topics: Aircraft Design, Testing and Performance Aerodynamic
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