Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig | Zendy

Zheng Gong | Zendy; Sergio A. Araujo-Estrada | Zendy; Mark Lowenberg | Zendy; Simon A. Neild | Zendy; Mikhail Goman | Zendy

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Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig

Author(s) -

Zheng Gong,

Sergio A. Araujo-Estrada,

Mark Lowenberg,

Simon A. Neild,

Mikhail Goman

Publication year - 2019

Publication title -

journal of aircraft

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.64

H-Index - 94

eISSN - 1533-3868

pISSN - 0021-8669

DOI - 10.2514/1.c034995

Subject(s) - stall (fluid mechanics) , aerodynamics , wind tunnel , angle of attack , control theory (sociology) , longitudinal static stability , aerodynamic force , aerospace engineering , mechanics , engineering , computer science , physics , control (management) , artificial intelligence

The high-incidence aerodynamics of a lightweight jet trainer aircraft model has been investigated using a novel five-degree-of-freedom (DOF) dynamic maneuver rig, recently updated with improved act...

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