The BASS code, a nonlinear high-order prefactored compact code is validated on a benchmark problem. The nonlinear response of a loaded airfoil to an impinging vertical gust is investigated in the parametric space of gust intensity and frequency. Computational resources, involving a Linux cluster, were set up and maintained. The code was corrected and adapted to this particular problem. Results are compared with linear solution from the GUST3D solver.
","abstract_html":"<p>The BASS code, a nonlinear high-order prefactored compact code is validated on a benchmark problem. The nonlinear response of a loaded airfoil to an impinging vertical gust is investigated in the parametric space of gust intensity and frequency. Computational resources, involving a Linux cluster, were set up and maintained. The code was corrected and adapted to this particular problem. Results are compared with linear solution from the GUST3D solver.</p>","abstract_has_math":false,"creators":["Lessiau, Claire M."],"institution":null,"degree_name":"Master of Science in Aerospace Engineering","degree_level":"Thesis - Open Access","degree_discipline":"Aerospace Engineering","degree_department":null,"school":null,"contributors":["Vladimir V. Golubev","Eric Perrell","Axel Rohde"],"advisors":[],"committee_chairs":[],"committee_members":[],"year":2003,"date_issued":"2003-07-01T07:00:00Z","date_published":"2003-07-01T07:00:00Z","updated_at":"2026-07-27T19:25:29Z","subjects":["numerical analysis","airfoil","impinging","gust","Aerospace Engineering"],"languages":[],"rights":[],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"https://commons.erau.edu/db-theses/120","outbound_label":"Repository record","outbound_source":"dc:identifier"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor","label":"Contributor","values":["Vladimir V. Golubev","Eric Perrell","Axel Rohde"]},{"key":"dc:creator","label":"Author","values":["Lessiau, Claire M."]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"thesis:degree_discipline","label":"Discipline","values":["Aerospace Engineering"]},{"key":"thesis:degree_level","label":"Degree Level","values":["Thesis - Open Access"]},{"key":"thesis:degree_name","label":"Degree Name","values":["Master of Science in Aerospace Engineering"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["numerical analysis","airfoil","impinging","gust","Aerospace Engineering"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://commons.erau.edu/db-theses/120"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["The BASS code, a nonlinear high-order prefactored compact code is validated on a benchmark problem. The nonlinear response of a loaded airfoil to an impinging vertical gust is investigated in the parametric space of gust intensity and frequency. Computational resources, involving a Linux cluster, were set up and maintained. The code was corrected and adapted to this particular problem. Results are compared with linear solution from the GUST3D solver.
"]},{"key":"dc:title","label":"Title","values":["Numerical Analysis of an Airfoil Response to an Impinging Gust"]}]}],"canonical_facts":{"dc:contributor":["Vladimir V. Golubev","Eric Perrell","Axel Rohde"],"dc:creator":["Lessiau, Claire M."],"dc:description.abstract":["The BASS code, a nonlinear high-order prefactored compact code is validated on a benchmark problem. The nonlinear response of a loaded airfoil to an impinging vertical gust is investigated in the parametric space of gust intensity and frequency. Computational resources, involving a Linux cluster, were set up and maintained. The code was corrected and adapted to this particular problem. Results are compared with linear solution from the GUST3D solver.
"],"dc:identifier":["https://commons.erau.edu/db-theses/120"],"dc:subject":["numerical analysis","airfoil","impinging","gust","Aerospace Engineering"],"dc:title":["Numerical Analysis of an Airfoil Response to an Impinging Gust"],"thesis:degree_discipline":["Aerospace Engineering"],"thesis:degree_level":["Thesis - Open Access"],"thesis:degree_name":["Master of Science in Aerospace Engineering"]},"updated_at":"2026-07-27T19:25:29Z"}