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Pages 137-143

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From page 137...
... 12.3.2. Tire and Arrestor Simulations As with the glass foam material evaluation, the arrestor models were constructed in LS-DYNA using the deformable FEM tire models and SPH arrestor beds (Figure 12-4)
From page 138...
... 12.3.2.1. Arrestor Bed Models The arrestor bed models were constructed using halfsymmetry to reduce computation time.
From page 139...
... Aircraft Landing Gear Tire Designation Included in Evaluation Main Gear H29x9.0-15 Included CRJ-200 Nose Gear R18x4.4 - Main Gear H44.5x16.5-21 Included B737-800 Nose Gear H27x7.7-15 - Main Gear H49x19-22 - B747-400 Nose Gear H49x19-22 - Table 12-1. FEM tire library for glass foam arrestor models.
From page 140...
... Metamodel Method The output from the batch simulations was extracted and assembled automatically by LS-OPT, where metamodels were constructed for the drag and vertical load forces. Metamodeling is analogous to fitting a curve through experimental data except that it is applied to multi-dimensional data sets.
From page 141...
... reflected similar trends. The right hand image of Figure 12-8 shows an interesting behavior: for the linear gradient material, the response becomes insensitive to the arrestor bed depth, becoming essentially flat in the depth-wise direction.
From page 142...
... 12.4.6. Summary of Metamodel Analysis The metamodel analysis explored linear, quadratic, and exponential depth-varying material profiles using stratified arrestor bed models.
From page 143...
... In practice, this methodology could be readily implemented using a glass foam block material, with minimal impact on anticipated cost, construction methods, or maintenance needs. Finally, Chapter 11 demonstrated that the exponentially depth-varying aggregate foam material could achieve performance leveling between aircraft.


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