NUMERICAL SIMULATION OF SUPERSONIC FLOW AROUND WING-BODY CONFIGURATION WITH INTEGRATED ENGINE NACELLE

@inproceedings{Kanazaki2001NUMERICALSO,
  title={NUMERICAL SIMULATION OF SUPERSONIC FLOW AROUND WING-BODY CONFIGURATION WITH INTEGRATED ENGINE NACELLE},
  author={Masahiro Kanazaki and Shigeru Obayashi and Kazuhiro Nakahashi},
  year={2001}
}
This paper presents numerical simulation of flowfields around a supersonic transport aircraft with an integrated engine nacelle. In this study, flowfields were simulated by solving the Euler equations with the unstructured grid method for handling the complex geometry. To simulate intake flows at actual flights, a bump was introduced inside the nacelle. The effect of nacelle mass flow ratios on overall aerodynamic performance was investigated in detail by changing bump heights. The spillage… CONTINUE READING

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