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TITLE : SIMULATION OF A SIDE CRUSH OF A DODGE NEON BIW AIM : Simulate the frontal crush of the dodge neon on a rigid wall and to post proccess the forces generated or transfer through specific cross-sectional areas of the car using Hypermesh (Radioss) and Hypercrush. A crash test is a form of destructive…
Leslie Enos
updated on 09 Oct 2020
TITLE : SIMULATION OF A SIDE CRUSH OF A DODGE NEON BIW
AIM : Simulate the frontal crush of the dodge neon on a rigid wall and to post proccess the forces generated or transfer through specific cross-sectional areas of the car using Hypermesh (Radioss) and Hypercrush.
A crash test is a form of destructive testing usually performed in order to ensure safe design standards in crashworthiness and crash compatibility for various modes of transportation (see automobile safety) or related systems and components.
Full Car Model
Reduced Frontal car
UNIT SYSTEM
The unit system which was used in this model was kg ms mm
PROCEDURE
CONTACT INTERFACE
A self contact is created for the car using the Type 7. All parts are selected as its a self contact interface interaction Properties used can be seen below.
PENETRATION AND CONNECTIVITY CHECK
it is very important to check for element which have penetrated into the gap because this can affect the simulations results and drops to negative. The simulation becomes unstable. Below is an image of the penetration check in hypercrush. As it can be seen there where no penetration found in the model.Also checked below is the connectivity of all parts and ther was no unconnected parts.
Isolating these parts, 1D elements are created on these parts to establish all neccesory connections. An example is shown below of connections on the rails.
RIGID WALL CREATION
Rigid wall is a body with very high stiffness and is made to be static and to receive the side crush of the dodge. The cordinates of the rigid wall is defined first by picking a node on the door to specify the tail cordinates. The head cordinates is created by copying that of the tail and only giving a little gap to the normal direction. This gap is defined as small as possible in order to reduce CPU computing time during simulation.The search distance of possible slave nodes that could hit the rigis wall is be selected together with a search tolerance. 0.1 sliding frequency is selected for the wall.
MASS BALANCING
iT IS IMPORTANT TO CONTROL THE DISTRIBUTION OF MASS IN THE MODEL TO REFLECT THE ACTUAL POSITION OF THE C.O.G OF THE FULL MODEL OF THE CAR. The full model of the car has its centre of gravity somewhere closer to the front drivers seat. Masses are added at the front and back links to push the COG to the middle part of the car.This masses must also be added to reach a desired weight of 700kg. The current weight before balancing was 166kg. 500kg was added to the front links and 34kg is added to the side links. The centre of gravity can be seen in place as a dot in the car model below.
INITIAL VELOCITY
Intial velocity kinematic condition of 35mph is added to propel the model horixontally in the x direction to the rigid wall to simulate the crush , with a friction of 0.1
CREATION OF CROSS-SECTION
Cross-sections are created for specific parts in order to study the force distribution in these parts. Parts are listed below
TIME STEP
Custom time step is specified with the following parameter
CREATING TH OUTPUT REQUEST
In order to post proccese the results of the simulation , the required data must be rquested. It can be seen below the requested uotput file ad the variables selected is left at default (DEF). All the sections are requested together. Intrusions at certain locations with a reference skew
CREATION OF ANIMATION OUTPUT REQUEST
In order to post proccese the results of the simulation , the required data must be rquested. The animation of vonmisses ,hourglass and specific energy, Time step and Mass variation is request by creating with ANIM_ELTYPE_RESTYPE.
MODEL QUALITY CHECK
It is important to check for possible errors that may occur during simulation and model checker shows all the errors together with warnings. Below it can be seen that no errors was seen during this check.
TIMESTEP AND ENERGY ERROR DEBUGGING
The time step through the simulation was as expected with the minimum time step not less than 0.0001ms and the energy error was well below 15%. Overall the mass change with a percentage of 0.000% . There was no change in mass during the simulation.
POST PROCCESING ANIMATION OUTPUT
ANIMATION
ANIMATION_SIDE
ANIMATION_FRONT
ENERGY TIME DATA
The flow of energy through the simulation was fairly as expected . The kinetic energy decreasing with significant increase in internal energy with time.Because energy absorption is the goal ,the whole of K.E which starts at the highest value should get dissipated and transferred to the internal energy. The more internal energy the more the deformation of the components. The copntact energy which is the energy spent in moving penetrations out of the gap zone is almost constant with a slight increase. This is good as its supposed to be less than 0 to 5% of the total energy. The total energy was slightly decreasing due to the loss of energy and this is expected from the negative energy error recorded. This is due to the timestep control of using CST applying small strain switching element deformation. Hourglass is well stabilized as its seen constant.
MASS PLOT
Overall the mass change with a percentage of 0.000% . There was no change in mass during the simulation.
TIME-STEP PLOT
Has it can be seen from the diagram above , there are some fluctuations in the time steps. There was a decrease early on at 10ms but the was increase as the simultions went on. At the end of the simulations the timestep decreased. This decrease is acceptable because the timestep was well above the critical time step value.
The time step was kept above the critcal value of 0.0001ms.
Energy error of -2.0 was recorded this indicates some energy being dissipated
Simulation Time = 9522.63 s
No of cycles = 340756
CROSS-SECTIONAL FORCES
CROSS_MEMBER_1
From the cross_member_1 where the driver's front seat is loacated, this crush resulted in a normal(Y) force of 10KN at 60ms from the crush.
CROSS_MEMBER_2
From the cross_member_2 the crush resulted in a normal(Y) force of 10KN at 18ms from the crush. This is due to the fact that the second crossmember was closer to the rigid wall and started deformation before the member_1.
Fuel_Tank_Intrusions
From 0 the intrusions into the fuel tank are was 270mm. The negative sign is due to the direction of the refernce skew created.
Hinge_PIllar_Intrusions
From 0 the intrusions into the fuel tank are was 224mm. The negative sign is due to the direction of the refernce skew created.
B_Pillar_Intrusions
From 0 the intrusions into the fuel tank are was 550mm. The negative sign is due to the direction of the refernce skew created.
Inner_Door_Intrusion_Velocity
The peak velocity of the door was 15mm/ms at the early stages but upon impact began to decrease due to the rigid bodies presence. The velocity reduced by 87% during crush.
CONCLUSION
The side crush was performed successfully with mass ,timestep an energy value all being balanced with errors. The B_pillar received the most forces upon impact and can be fatal for any occupant therefore the stiffness of that should be increased by improving the material used. The intrusion by the hinge and fuel need to be reduced by adding more components such as beams, absorbtion pads and cross rods to absorb more energy before they reach these critical areas.
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