| contributor author | Guo, Jiangling | |
| contributor author | Gu, Yunsong | |
| contributor author | Li, Linkai | |
| contributor author | Wang, Shilong | |
| contributor author | Zhang, Yuzhe | |
| date accessioned | 2026-08-20T21:13:00Z | |
| date available | 2026-08-20T21:13:00Z | |
| date copyright | 2025/06/06 | |
| date issued | 2025 | |
| identifier other | JAEEEZ.ASENG-6178.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314127 | |
| description abstract | AbstractAt 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 ... | |
| publisher | American Society of Civil Engineers | |
| title | Normal Force and Pitching Moment Trend Sensing of Delta Wing Based on Flow Physical Topology with Sparse Pressure Measurements | |
| type | Journal Article | |
| journal volume | 38 | |
| journal issue | 5 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/JAEEEZ.ASENG-6178 | |
| journal fristpage | 04025064-1 | |
| journal lastpage | 04025064-13 | |
| page | 13 | |
| tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005 | |
| contenttype | Fulltext | |