Dieter Hachenberg

发表

AN APPROACH TO MODELLING AND PREDICTING IMPACT DAMAGE IN COMPOSITE STRUCTURES

Murray L. Scott, Sagar P. Rajbhandari, Rodney S. Thomson, 2002 .

The Kinematics Model - A Numerical Method for the Development of a Crashworthy Composite Fuselage Design of Transport Aircraft

Matthias Waimer, Dieter Kohlgrüber, Heinz Voggenreiter, 2010 .

Simulation of impact on sandwich structures

Murray L. Scott, R. S. Thomson, Dieter Hachenberg, 2005 .

The analysis of skin-to-stiffener debonding in composite aerospace structures

Murray L. Scott, Rodney S. Thomson, Dieter Hachenberg, 2002 .

Dynamic Component Testing on CFRP Crash Absorbers of a Transport Aircraft Sub-Cargo Structure

Matthias Waimer, Dieter Kohlgrüber, Heinz Voggenreiter, 2012 .

Development of a Crashworthy Composite Fuselage Design Using a Kinematics Model

Matthias Waimer, Dieter Kohlgrüber, Heinz Voggenreiter, 2010 .

Experimental study of CFRP components subjected to dynamic crash loads

Matthias Waimer, Dieter Kohlgrüber, Heinz Voggenreiter, 2013 .

Influence of post-buckling behaviour of composite stiffened panels on the damage criticality

Murray L. Scott, Rodney S. Thomson, Dieter Hachenberg, 2004 .