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Optimization design for bird strike resistance of blended-wing-body civil aircraft cabin doors

  • Northwestern Polytechnical University Xian

Research output: Contribution to journalArticlepeer-review

Abstract

The Blended Wing Body (BWB) configuration in civil aviation represents a major leap in aerodynamic performance, achieved through the seamless integration of fuselage and wing structures—effectively breaking through the design constraints of conventional “tube-and-wing” aircraft. Yet, this architectural innovation brings new challenges: the flattened fuselage places cabin doors directly on the windward surface, increasing the risk of cabin depressurization following bird impacts. Current airworthiness regulations (e.g., CCAR-25.365) lack specific provisions regarding bird strike resistance for cabin doors, and thus, traditional protective strategies are not readily transferrable to BWB designs. To address this, a Finite Element (FE) model was constructed for the BWB cabin door, incorporating the Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS). Upon validating its static strength under extreme loading conditions, a surrogate model was established, enabling multi objective optimization using Latin Hypercube Sampling (LHS) and the Non-dominated Sorting Genetic Algorithm II (NSGA-II) algorithm. This optimization yielded a 23.27% mass reduction, with a 10.28% increase in the Tsai-Wu failure factor. Furthermore, a coupled Smoothed Particle Hydrodynamics-Finite Element Method (SPH-FEM) numerical approach was employed to simulate the bird strike scenario involving a 3.6 kg bird traveling at 140 m/s at an incidence angle of 18.43°. To bolster impact resistance, structural enhancements were introduced using 7075-T351 aluminum alloy doublers around the door and adjacent cutouts. These enhancements were further refined via a Multi-island Genetic Algorithm (GA), resulting in an additional 32.20% reduction in reinforcement mass. The post-optimization analysis confirmed the absence of perforation damage and plastic deformation in the door locking system and kinematic linkage. This research establishes a novel framework for assessing bird strike resilience in BWB cabin doors, contributing foundational data to airworthiness certification and offering practical reference for subsequent experimental validations.

Original languageEnglish
Article number110953
JournalEngineering Failure Analysis
Volume194
DOIs
StatePublished - 1 Sep 2026

Keywords

  • BWB civil aircraft cabin door
  • Bird strike
  • Bird strike reinforcement
  • Designoptimization
  • SPH

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