{"id":"https://openalex.org/W7083465569","doi":"https://doi.org/10.14459/2025md1760398","title":"Aerodynamic Design and Performance Analysis of a Morphing Wing Racing Sailplane","display_name":"Aerodynamic Design and Performance Analysis of a Morphing Wing Racing Sailplane","publication_year":2025,"publication_date":"2025-09-24","ids":{"openalex":"https://openalex.org/W7083465569","doi":"https://doi.org/10.14459/2025md1760398"},"language":"en","primary_location":{"id":"pmh:oai:aleph.bib-bvb.de:BVB01-035802279","doi":null,"is_oa":false,"landing_page_url":"https://mediatum.ub.tum.de/?id=1760398","pdf_url":null,"source":null,"license":null,"license_id":null,"version":"submittedVersion","is_accepted":false,"is_published":false,"raw_source_name":null,"raw_type":"Hochschulschrift"},"volume":null,"type":"dissertation","indexed_in":["datacite"],"open_access":{"is_oa":true,"oa_status":"green","oa_url":"https://doi.org/10.14459/2025md1760398","any_repository_has_fulltext":true},"authorships":[{"author_position":"first","author":{"id":"https://openalex.org/A5009356186","display_name":"Johannes Achleitner","orcid":"https://orcid.org/0000-0002-5476-4589","observed_orcids":["https://orcid.org/0000-0002-5476-4589"]},"institutions":[],"countries":[],"is_corresponding":true,"raw_author_name":"Achleitner, Johannes","raw_affiliation_strings":[],"raw_orcid":null,"affiliations":[]}],"institutions":[],"countries_distinct_count":0,"institutions_distinct_count":0,"corresponding_author_ids":["https://openalex.org/A5009356186"],"corresponding_institution_ids":[],"apc_list":null,"apc_paid":null,"fwci":null,"has_fulltext":false,"cited_by_count":0,"citation_normalized_percentile":null,"cited_by_percentile_year":null,"biblio":{"volume":null,"issue":null,"first_page":null,"last_page":null},"is_retracted":false,"is_paratext":false,"is_xpac":true,"primary_topic":{"id":"https://openalex.org/T11096","display_name":"Aeroelasticity and Vibration Control","score":0.9663000106811523,"subfield":{"id":"https://openalex.org/subfields/2202","display_name":"Aerospace Engineering"},"field":{"id":"https://openalex.org/fields/22","display_name":"Engineering"},"domain":{"id":"https://openalex.org/domains/3","display_name":"Physical Sciences"}},"topics":[{"id":"https://openalex.org/T11096","display_name":"Aeroelasticity and Vibration Control","score":0.9663000106811523,"subfield":{"id":"https://openalex.org/subfields/2202","display_name":"Aerospace Engineering"},"field":{"id":"https://openalex.org/fields/22","display_name":"Engineering"},"domain":{"id":"https://openalex.org/domains/3","display_name":"Physical Sciences"}},{"id":"https://openalex.org/T11524","display_name":"Advanced Aircraft Design and Technologies","score":0.023099999874830246,"subfield":{"id":"https://openalex.org/subfields/2306","display_name":"Global and Planetary Change"},"field":{"id":"https://openalex.org/fields/23","display_name":"Environmental Science"},"domain":{"id":"https://openalex.org/domains/3","display_name":"Physical Sciences"}},{"id":"https://openalex.org/T10173","display_name":"Computational Fluid Dynamics and Aerodynamics","score":0.0034000000450760126,"subfield":{"id":"https://openalex.org/subfields/2206","display_name":"Computational Mechanics"},"field":{"id":"https://openalex.org/fields/22","display_name":"Engineering"},"domain":{"id":"https://openalex.org/domains/3","display_name":"Physical Sciences"}}],"keywords":[{"id":"https://openalex.org/keywords/morphing-wing","display_name":"morphing wing","score":0.9739999771118164},{"id":"https://openalex.org/keywords/gliders","display_name":"gliders","score":0.8820000290870667},{"id":"https://openalex.org/keywords/airfoil-design","display_name":"airfoil design","score":0.6489999890327454},{"id":"https://openalex.org/keywords/trailing-edge-flaps","display_name":"trailing edge flaps","score":0.7639999985694885},{"id":"https://openalex.org/keywords/lift-to-drag-ratio","display_name":"lift-to-drag ratio","score":0.718999981880188},{"id":"https://openalex.org/keywords/wing-loading","display_name":"wing loading","score":0.8270000219345093},{"id":"https://openalex.org/keywords/airfoil-shape-optimization","display_name":"airfoil shape optimization","score":0.5960000157356262},{"id":"https://openalex.org/keywords/geometry-parameterization","display_name":"geometry parameterization","score":0.9169999957084656}],"concepts":[{"id":"https://openalex.org/C97257150","wikidata":"https://www.wikidata.org/wiki/Q161358","display_name":"Wing","level":2,"score":0.8522999882698059},{"id":"https://openalex.org/C50637493","wikidata":"https://www.wikidata.org/wiki/Q1136781","display_name":"Morphing","level":2,"score":0.8489999771118164},{"id":"https://openalex.org/C112124176","wikidata":"https://www.wikidata.org/wiki/Q4698744","display_name":"Airfoil","level":2,"score":0.8046000003814697},{"id":"https://openalex.org/C13393347","wikidata":"https://www.wikidata.org/wiki/Q8424","display_name":"Aerodynamics","level":2,"score":0.5866000056266785},{"id":"https://openalex.org/C66938386","wikidata":"https://www.wikidata.org/wiki/Q633538","display_name":"Structural engineering","level":1,"score":0.5555999875068665},{"id":"https://openalex.org/C107779570","wikidata":"https://www.wikidata.org/wiki/Q887216","display_name":"Wing loading","level":4,"score":0.545799970626831},{"id":"https://openalex.org/C107157880","wikidata":"https://www.wikidata.org/wiki/Q845727","display_name":"Lift-to-drag ratio","level":3,"score":0.5180000066757202},{"id":"https://openalex.org/C28317120","wikidata":"https://www.wikidata.org/wiki/Q975211","display_name":"Trailing edge","level":2,"score":0.5062000155448914},{"id":"https://openalex.org/C127413603","wikidata":"https://www.wikidata.org/wiki/Q11023","display_name":"Engineering","level":0,"score":0.47999998927116394},{"id":"https://openalex.org/C2779570065","wikidata":"https://www.wikidata.org/wiki/Q1754137","display_name":"Leading edge","level":2,"score":0.45249998569488525},{"id":"https://openalex.org/C137990359","wikidata":"https://www.wikidata.org/wiki/Q1120746","display_name":"Wing twist","level":4,"score":0.4327999949455261},{"id":"https://openalex.org/C195637266","wikidata":"https://www.wikidata.org/wiki/Q1662148","display_name":"Lift-induced drag","level":4,"score":0.4323999881744385},{"id":"https://openalex.org/C146978453","wikidata":"https://www.wikidata.org/wiki/Q3798668","display_name":"Aerospace engineering","level":1,"score":0.42820000648498535},{"id":"https://openalex.org/C72921944","wikidata":"https://www.wikidata.org/wiki/Q206621","display_name":"Drag","level":2,"score":0.39559999108314514},{"id":"https://openalex.org/C150486481","wikidata":"https://www.wikidata.org/wiki/Q760106","display_name":"Lift coefficient","level":4,"score":0.3727000057697296},{"id":"https://openalex.org/C139002025","wikidata":"https://www.wikidata.org/wiki/Q3001212","display_name":"Lift (data mining)","level":2,"score":0.36970001459121704},{"id":"https://openalex.org/C60053565","wikidata":"https://www.wikidata.org/wiki/Q1021159","display_name":"Camber (aerodynamics)","level":2,"score":0.36800000071525574},{"id":"https://openalex.org/C71839028","wikidata":"https://www.wikidata.org/wiki/Q7972627","display_name":"Washout","level":2,"score":0.33799999952316284},{"id":"https://openalex.org/C207390838","wikidata":"https://www.wikidata.org/wiki/Q1929294","display_name":"Swept wing","level":3,"score":0.31850001215934753},{"id":"https://openalex.org/C41008148","wikidata":"https://www.wikidata.org/wiki/Q21198","display_name":"Computer science","level":0,"score":0.3165000081062317},{"id":"https://openalex.org/C199104240","wikidata":"https://www.wikidata.org/wiki/Q118291","display_name":"Marine engineering","level":1,"score":0.3091000020503998},{"id":"https://openalex.org/C86811826","wikidata":"https://www.wikidata.org/wiki/Q2992500","display_name":"Wing configuration","level":3,"score":0.30570000410079956},{"id":"https://openalex.org/C527307","wikidata":"https://www.wikidata.org/wiki/Q370906","display_name":"Angle of attack","level":3,"score":0.2806999981403351},{"id":"https://openalex.org/C189360488","wikidata":"https://www.wikidata.org/wiki/Q1577504","display_name":"NACA airfoil","level":4,"score":0.25609999895095825},{"id":"https://openalex.org/C2780129039","wikidata":"https://www.wikidata.org/wiki/Q1931107","display_name":"Section (typography)","level":2,"score":0.2549999952316284},{"id":"https://openalex.org/C1633027","wikidata":"https://www.wikidata.org/wiki/Q815820","display_name":"Computational fluid dynamics","level":2,"score":0.25360000133514404},{"id":"https://openalex.org/C127313418","wikidata":"https://www.wikidata.org/wiki/Q1069","display_name":"Geology","level":0,"score":0.2500999867916107}],"mesh":[],"locations_count":2,"locations":[{"id":"pmh:oai:aleph.bib-bvb.de:BVB01-035802279","doi":null,"is_oa":false,"landing_page_url":"https://mediatum.ub.tum.de/?id=1760398","pdf_url":null,"source":null,"license":null,"license_id":null,"version":"submittedVersion","is_accepted":false,"is_published":false,"raw_source_name":null,"raw_type":"Hochschulschrift"},{"id":"doi:10.14459/2025md1760398","doi":"https://doi.org/10.14459/2025md1760398","is_oa":true,"landing_page_url":"https://doi.org/10.14459/2025md1760398","pdf_url":null,"source":{"id":"https://openalex.org/S4377196330","display_name":"mediaTUM  (Technical University of Munich)","issn_l":null,"issn":null,"is_oa":false,"is_in_doaj":false,"is_core":false,"listed_in":[],"host_organization":"https://openalex.org/I62916508","host_organization_name":"Technical University of Munich","host_organization_lineage":["https://openalex.org/I62916508"],"host_organization_lineage_names":[],"type":"repository"},"license":null,"license_id":null,"version":null,"is_accepted":false,"is_published":null,"raw_source_name":null,"raw_type":"thesis"}],"best_oa_location":{"id":"doi:10.14459/2025md1760398","doi":"https://doi.org/10.14459/2025md1760398","is_oa":true,"landing_page_url":"https://doi.org/10.14459/2025md1760398","pdf_url":null,"source":{"id":"https://openalex.org/S4377196330","display_name":"mediaTUM  (Technical University of Munich)","issn_l":null,"issn":null,"is_oa":false,"is_in_doaj":false,"is_core":false,"listed_in":[],"host_organization":"https://openalex.org/I62916508","host_organization_name":"Technical University of Munich","host_organization_lineage":["https://openalex.org/I62916508"],"host_organization_lineage_names":[],"type":"repository"},"license":null,"license_id":null,"version":null,"is_accepted":false,"is_published":false,"raw_source_name":null,"raw_type":"thesis"},"sustainable_development_goals":[],"sustainable_development_goals_aurora":[{"id":"https://metadata.un.org/sdg/7","display_name":"Affordable and clean energy","score":0.8116564154624939}],"study_designs":[],"awards":[],"funders":[],"has_content":{"pdf":false,"grobid_xml":false},"content_urls":null,"referenced_works_count":0,"referenced_works":[],"related_works":[],"abstract_inverted_index":{"A":[0],"wing":[1,41,45,59],"with":[2,26],"a":[3,61,67],"morphing":[4,58],"forward":[5],"section":[6],"and":[7,20,32,43],"conventional":[8,37],"trailing":[9],"edge":[10],"flap":[11],"is":[12],"proposed":[13],"to":[14,28,36,52],"improve":[15],"sailplane":[16],"performance.":[17],"Novel":[18],"optimization":[19],"geometry":[21],"parameterization":[22],"methods":[23],"produce":[24],"airfoils":[25],"up":[27],"20%":[29],"higher":[30],"lift":[31],"similar":[33],"drag":[34],"compared":[35],"airfoils,":[38],"allowing":[39],"reduced":[40],"area":[42],"increased":[44],"loading":[46],"without":[47],"increasing":[48],"minimum":[49],"speed.":[50],"Applied":[51],"an":[53],"existing":[54],"18-meter":[55],"sailplane,":[56],"the":[57,77,80],"shows":[60],"3.4%":[62],"performance":[63],"increase":[64],"based":[65],"on":[66],"new":[68],"competition-based":[69],"metric.":[70],"Further":[71],"gains":[72],"are":[73],"possible":[74],"by":[75],"redesigning":[76],"tailplane":[78],"of":[79],"aircraft.":[81]},"counts_by_year":[],"updated_date":"2026-10-12T09:40:04.860316","created_date":"2025-10-10T00:00:00"}
