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    <responseDate>2026-10-14T03:42:42Z</responseDate>
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    <identifier>10.57760/sciencedb.j00145.0002w</identifier>
    <datestamp>2026-09-15T16:02:23Z</datestamp>
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  <dc:date>2026-09-15</dc:date>
  <dc:title>Numerical data and implementation for transient aeroelasticity of telescoping&amp;ndash;folding morphing wings using a geometric pressure-port Birkhoffian framework</dc:title>
  <dc:identifier>doi:10.57760/sciencedb.j00145.0002w</dc:identifier>
  <dc:language>en</dc:language>
  <dc:description>This collection contains numerical model archives, implementation snapshots, configuration files, readable data exports and table sources associated with five aeroelastic examples. They cover pressure-work and kinematic checks, Goland and three-segment flutter calculations, conservative formulation comparisons, actuator-limited responses, and dynamic, continuous-frozen and frozen-library comparisons. A separate benchmark archive contains operation counts and the original balanced timing observations. The pressure test uses a manufactured field; literature reference values are anchors, not measurements performed by the authors. The timing results apply to the recorded algorithms and hardware. No experimental or flight-test dataset is claimed. Local packaging checks included archive consistency, replay assessments, exact-input Case 1 reconstruction and a short benchmark count rerun, not full reruns of every expensive solver. See the README, array dictionary and per-case source snapshots for units, ordering, dependencies and reproduction commands.</dc:description>
  <dc:subject>Morphing wing; Aeroelasticity; Birkhoffian system; Pressure-power port; Power-consistent discretization</dc:subject>
  <dc:creator>Hao Luo</dc:creator>
  <dc:creator>Zhiping Qiu</dc:creator>
  <dc:creator>Yunlong Li</dc:creator>
  <dc:rights>PUBLIC</dc:rights>
  <dc:rights>https://creativecommons.org/licenses/by/4.0/</dc:rights>
  <dc:type>dataset</dc:type>
  <dc:publisher>Science Data Bank</dc:publisher>
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