{"id":{"repo_id":"maryland","oai_identifier":"oai:drum.lib.umd.edu:1903/21285"},"canonical_url":"https://search.dev.ndltd.org/etd/maryland/oai:drum.lib.umd.edu:1903/21285","repository":{"repo_id":"maryland","name":"University of Maryland","base_url":"https://api.drum.lib.umd.edu/server/oai/request"},"display":{"title":"MICRO AIR VEHICLE SCALE GUST-WING INTERACTION IN A WIND TUNNEL","abstract":"Studying isolated gust effects on simple airfoil models in a controlled environment is a necessity to further the development of MAV gust response and control laws. This work describes the creation of a vertical gust generator in a low speed, low turbulence wind tunnel through the use of an actuated fan placed below the tunnel and ducted through its floor. Gusts of up to 40% of the freestream velocity were created. Characterization of the gust generator is shown, and its interaction with a stationary wing at several angles of attack is evaluated. The actuated gust profile is also compared to that of a pitched wing in a gust-less environment with many visible similarities.","abstract_html":"Studying isolated gust effects on simple airfoil models in a controlled environment is a necessity to further the development of MAV gust response and control laws. This work describes the creation of a vertical gust generator in a low speed, low turbulence wind tunnel through the use of an actuated fan placed below the tunnel and ducted through its floor. Gusts of up to 40% of the freestream velocity were created. Characterization of the gust generator is shown, and its interaction with a stationary wing at several angles of attack is evaluated. The actuated gust profile is also compared to that of a pitched wing in a gust-less environment with many visible similarities.","abstract_has_math":false,"creators":["Smith, Zachary Francis"],"institution":null,"degree_name":null,"degree_level":null,"degree_discipline":null,"degree_department":"Aerospace Engineering","school":null,"contributors":[],"advisors":["Jones, Anya R","Hrynuk, John T"],"committee_chairs":[],"committee_members":[],"year":2018,"date_issued":"2018","date_published":"2018","updated_at":"2026-07-24T03:02:24Z","subjects":[],"languages":["en"],"rights":[],"rights_urls":[],"identifier_entries":[{"key":"dc:identifier","label":"Identifier","values":["https://doi.org/10.13016/M2Z60C563"],"render_values":[{"text":"https://doi.org/10.13016/M2Z60C563","href":"https://doi.org/10.13016/M2Z60C563","code":true}]}]},"links":{"outbound_url":"http://hdl.handle.net/1903/21285","outbound_label":"Handle","outbound_source":"dc:identifier.uri"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor.advisor","label":"Advisor","values":["Jones, Anya R","Hrynuk, John T"]},{"key":"dc:contributor.department","label":"Department","values":["Aerospace Engineering"]},{"key":"dc:creator","label":"Author","values":["Smith, Zachary Francis"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date.accessioned","label":"Dc Date Accessioned","values":["2018-09-12T05:57:09Z"]},{"key":"dc:date.available","label":"Dc Date Available","values":["2018-09-12T05:57:09Z"]},{"key":"dc:date.issued","label":"Date","values":["2018"]},{"key":"dc:type","label":"Dc Type","values":["Thesis"]}]},{"id":"language_rights","label":"Language and Rights","entries":[{"key":"dc:language.iso","label":"Language (ISO)","values":["en"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier","label":"Identifier","values":["https://doi.org/10.13016/M2Z60C563"]},{"key":"dc:identifier.uri","label":"Identifier URI","values":["http://hdl.handle.net/1903/21285"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["Studying isolated gust effects on simple airfoil models in a controlled environment is a necessity to further the development of MAV gust response and control laws. This work describes the creation of a vertical gust generator in a low speed, low turbulence wind tunnel through the use of an actuated fan placed below the tunnel and ducted through its floor. Gusts of up to 40% of the freestream velocity were created. Characterization of the gust generator is shown, and its interaction with a stationary wing at several angles of attack is evaluated. The actuated gust profile is also compared to that of a pitched wing in a gust-less environment with many visible similarities."]},{"key":"dc:title","label":"Title","values":["MICRO AIR VEHICLE SCALE GUST-WING INTERACTION IN A WIND TUNNEL"]}]}],"canonical_facts":{"dc:contributor.advisor":["Jones, Anya R","Hrynuk, John T"],"dc:contributor.department":["Aerospace Engineering"],"dc:creator":["Smith, Zachary Francis"],"dc:date.accessioned":["2018-09-12T05:57:09Z"],"dc:date.available":["2018-09-12T05:57:09Z"],"dc:date.issued":["2018"],"dc:description.abstract":["Studying isolated gust effects on simple airfoil models in a controlled environment is a necessity to further the development of MAV gust response and control laws. This work describes the creation of a vertical gust generator in a low speed, low turbulence wind tunnel through the use of an actuated fan placed below the tunnel and ducted through its floor. Gusts of up to 40% of the freestream velocity were created. Characterization of the gust generator is shown, and its interaction with a stationary wing at several angles of attack is evaluated. The actuated gust profile is also compared to that of a pitched wing in a gust-less environment with many visible similarities."],"dc:identifier":["https://doi.org/10.13016/M2Z60C563"],"dc:identifier.uri":["http://hdl.handle.net/1903/21285"],"dc:language.iso":["en"],"dc:title":["MICRO AIR VEHICLE SCALE GUST-WING INTERACTION IN A WIND TUNNEL"],"dc:type":["Thesis"]},"updated_at":"2026-07-24T03:02:24Z"}