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propulsion

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CFD simulation of an aeroacoustic oscillating resonator using the Lattice Boltzmann Method (D2Q9). Visualise thrust generation via dynamic boundary layer and asymmetric fluid resistance accumulation.

  • Updated Jul 27, 2026
  • Python

Advanced rocket trajectory simulation and design optimization system with parallel optimization algorithms and supersonic flight regime detection. Optimizes diameter, nose cone length, and body length to achieve target apogee within tolerance.

  • Updated May 13, 2026
  • Python

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