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contributor authorGuo, Jiangling
contributor authorGu, Yunsong
contributor authorLi, Linkai
contributor authorWang, Shilong
contributor authorZhang, Yuzhe
date accessioned2026-08-20T21:13:00Z
date available2026-08-20T21:13:00Z
date copyright2025/06/06
date issued2025
identifier otherJAEEEZ.ASENG-6178.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314127
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 ...
publisherAmerican Society of Civil Engineers
titleNormal Force and Pitching Moment Trend Sensing of Delta Wing Based on Flow Physical Topology with Sparse Pressure Measurements
typeJournal Article
journal volume38
journal issue5
journal titleJournal of Aerospace Engineering
identifier doi10.1061/JAEEEZ.ASENG-6178
journal fristpage04025064-1
journal lastpage04025064-13
page13
treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005
contenttypeFulltext


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