31st Aerospace Sciences Meeting 1993
DOI: 10.2514/6.1993-522
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Juncture flow improvement for wing/pylon configurations by using CFDmethodology

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“…The flow over the final pylon design was measured during flight test and validated with a Navier-Stokes flow solver. Gea et al [59] improved an existing wing-pylon configuration by employing a Chimera-based Navier-Stokes flow solver.…”
Section: Transonic Flowmentioning
confidence: 99%
“…The flow over the final pylon design was measured during flight test and validated with a Navier-Stokes flow solver. Gea et al [59] improved an existing wing-pylon configuration by employing a Chimera-based Navier-Stokes flow solver.…”
Section: Transonic Flowmentioning
confidence: 99%