Abstract
The spatial distribution of magnetic nanofillers within fibrous carbon scaffolds determines both impedance matching and broadband attenuation, yet the aerodynamic forces governing filler rearrangement during spinning remain unexploited as a design variable. We demonstrate that an L-shaped precursor needle within a solution blow spinning nozzle generates asymmetric aerodynamic shear. This shear converts the near-nozzle gas flow from a symmetric annular jet into a localized asymmetric forcing field. Large-eddy simulations reveal gas-phase shear rates above 3.0 × 105 s−1 and coherent vortical structures absent in conventional nozzles. The near-nozzle extensional stress exceeds the van der Waals cohesion of Co@BCN bundles, consistent with the disaggregated cobalt domains observed after carbonization. Post-carbonization electron microscopy and elemental mapping reveal discrete cobalt domains within the carbon nanofiber matrix, a configuration that enhances interfacial polarization while suppressing percolative conductivity. At 10 wt.% filler loading in the paraffin matrix, the optimized Co@BCN-CF-2 achieves a minimum reflection loss of −69.4 dB at 8.08 GHz (3.4 mm). The effective absorption bandwidth reaches 5.2 GHz (2.2 mm), and the simulated radar cross-section reduction attains 20.98 dB. These findings establish near-nozzle aerodynamic forcing as a demonstrated, tunable processing variable for filler-domain assembly in the present Co@BCN/PAN SBS nanofiber system.
| Original language | English |
|---|---|
| Article number | e77369 |
| Journal | Advanced Functional Materials |
| Volume | 36 |
| Issue number | 68 |
| DOIs | |
| State | Published - 24 Aug 2026 |
| Externally published | Yes |
Keywords
- asymmetric aerodynamic shear
- electromagnetic wave absorption
- impedance matching
- magnetic-dielectric composites
- solution blow spinning
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