2005
DOI: 10.2514/1.5440
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Control Surface Response of a Blended Wing Body Aeroelastic Wind-Tunnel Model

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Cited by 5 publications
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“…Seidler et al investigated a surrogate model for the prediction of response, which is less expensive compared to Reynolds-Averaged Navier Stokes equations [32]. Carlsson [29] and Phillips [34] performed experimental tests of transient deployment of mechanical control surfaces.…”
Section: Introductionmentioning
confidence: 99%
“…Seidler et al investigated a surrogate model for the prediction of response, which is less expensive compared to Reynolds-Averaged Navier Stokes equations [32]. Carlsson [29] and Phillips [34] performed experimental tests of transient deployment of mechanical control surfaces.…”
Section: Introductionmentioning
confidence: 99%