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dc.contributor.authorGuo, Jiangling
dc.contributor.authorGu, Yunsong
dc.contributor.authorLi, Linkai
dc.contributor.authorWang, Shilong
dc.contributor.authorZhang, Yuzhe
dc.date.accessioned2026-08-20T21:13:00Z
dc.date.available2026-08-20T21:13:00Z
dc.date.copyright2025/06/06
dc.date.issued2025
dc.identifier.otherJAEEEZ.ASENG-6178.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314127
dc.description.abstractAbstractAt high angles of attack (AOAs), aircraft experience significant nonlinear aerodynamic forces, which are influenced predominantly by vortex structures. These unsteady forces and moments have a considerable impact on aircraft maneuverability and ...Practical ApplicationsModern aircraft frequently require significant angles of attack during line-of-sight combat operations. The swift variation in attitude angle triggers an immediate shift in the adjacent flow field, making the aircraft susceptible to ...
dc.publisherAmerican Society of Civil Engineers
dc.titleNormal Force and Pitching Moment Trend Sensing of Delta Wing Based on Flow Physical Topology with Sparse Pressure Measurements
dc.typeJournal Article
dc.journal.volume38
dc.journal.issue5
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6178
dc.journal.fristpage04025064-1
dc.journal.lastpage04025064-13
dc.page13
dc.treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005
dc.contenttypeFulltext


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