Kindervater, Christof (2006) Helicopter and Aircraft Structures under Extreme Crash and High Velocity Impact - Trends of Structural Concepts and Numetrical Simulation.
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The paper reports on the recent trends in crashworthiness (CW) and High Velocity Impact (HVI) substantiation of transport A/C and helicopters by means of numerical simulation with explicit crash/HVI-codes such as PAM-CRASH/-SHOCK or LSDYNA where the simulations are used to support concept, design, and certification phases. Various presented aspects of crashworthiness and HVI comprise structural concepts and energy absorbing (EA) behaviour of composite airframe structures, HVI loading of composite aircraft structural components, the water impact environment of helicopters and ditching behaviour of A/C, and the interaction of the occupant with the crashing vehicle.
|Title:||Helicopter and Aircraft Structures under Extreme Crash and High Velocity Impact - Trends of Structural Concepts and Numetrical Simulation|
|Date:||14 September 2006|
|In ISI Web of Science:||No|
|Keywords:||Crashworthiness, High Velocity Impact (HVI), Transport Aircraft, helicopter, numerical simulation, explicit crash-/HVI codes, ernergy absorption, composite airframe structures, water impact, ditching|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Rotorcraft, Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L RR - Rotorcraft Research, L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Structures & Materials, L - The Robust Rotorcraft|
|Institutes and Institutions:||Institute of Structures and Design > Structural Integrity|
|Deposited By:||Christof Kindervater|
|Deposited On:||16 Jan 2007|
|Last Modified:||27 Apr 2009 13:26|
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