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Aircraft Design, Testing and Performance

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ATTAS


The flight test bed VFW614/ATTAS is based on the two engine, short haul, 44-seats passenger jet VFW614, which was developed and built in the seventies in Bremen/Germany by the VFW-Fokker company (toda...
 http://www.dlr.de/fb/en/desktopdefault.aspx/tabid-3707/5786_read-8393/
Related Topics: Aircraft Design, Testing and Performance Avionics and Aircraft Instrumentation Aircraft Stability and Control

Successful Experiment Series under Weightlessness


Scientists from the DLR’s Institute of Composite Structures and Adaptive Systems performed several experiments onboard of the A300 Zero-G test aircraft, at February 13th. This flying test laborato...
 http://www.dlr.de/fa/en/desktopdefault.aspx/tabid-1330/1811_read-15990/
Related Topics: Aircraft Design, Testing and Performance Spacecraft Propulsion and Power Communications and Radar Fluid Mechanics and Thermodynamics System Analysis Qualification

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: Aerodynamic Aircraft Design, Testing and Performance Aircraft Stability and Control Structural Mechanics

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 Design, Testing and Performance Aircraft Stability and Control Numerical Analysis
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