Advances in aircraft and spacecraft science

  • 제9권5호
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  • Pages.479-491
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  • 2022
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  • 2287-528X(pISSN)
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  • 2287-5271(eISSN)
테크노프레스 (Techno-Press)
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Q1D modeling of hydrodynamic instabilities in solid rocket motors

  • M., Grossi (Department of Mechanical and Aerospace Engineering, Sapienza University of Rome) ;
  • D., Bianchi (Department of Mechanical and Aerospace Engineering, Sapienza University of Rome) ;
  • B., Favini (Department of Mechanical and Aerospace Engineering, Sapienza University of Rome)
  • 투고 : 2022.02.25
  • 심사 : 2022.09.12
  • 발행 : 2022.09.25
⟨ 이전 논문 다음 논문 ⟩

초록

This work concerns the investigation of a Q1D methodology employed to study pressure oscillations in solid rocket motors driven by hydrodynamic instabilities. A laboratory-scale solid motor designed to develop vortex-shedding phenomena is analyzed for the whole firing time. The comparison between numerical results and experimental data shows good agreement regarding pressure oscillations signature, especially in the flute-mode behavior, the typical oscillations frequency trend present in any motor liable to hydrodynamic instabilities. Such result ensures the model capability to cope with this particular kind of pressure oscillations source, allowing the investigation of the phenomenon with a lighter and cost savings methodology than CFD simulations.

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참고문헌

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