Surrogate model development for optimized blended-wing-body aerodynamics

In the conceptual design phase of conventional-configuration aircraft, calibrated low-fidelity methods provide sufficiently accurate estimates of aerodynamic coefficients. It has been observed, however, that for blended-wing-body aircraft, important flow effects are not captured adequately with low-...

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Veröffentlicht in:Journal of aircraft 2022-09
Hauptverfasser: Aubeelack, Hema, Segonds, Stéphane, Bes, Christian, Druot, Thierry, Brezillon, Joël, Bérard, Adrien, Duffau, Marylène, Gallant, Guillaume
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Sprache:eng
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