On wire-driven parallel suspension systems for static and dynamic derivatives of aircraft in low-speed wind tunnels

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 30, Issue 8, 2009, Pages 1549-1554

  Zheng, Yaqing ^a,b   Lin, Qi ^a   Liu, Xiongwei ^c   Peter, Mitrouchev ^d  

^a XIAMEN UNIVERSITY   (China)

^b HUAQIAO UNIVERSITY   (China)

^c UNIVERSITY OF CENTRAL LANCASHIRE   (United Kingdom)

^d LABORATOIRE G SCOP   (France)

Author keywords

Dynamic derivative; Static derivative; Suspension system; Wind tunnel; Wire driven

Indexed keywords

DYNAMIC DERIVATIVE; DYNAMIC DERIVATIVES; EXPERIMENTAL ASPECTS; LOW-SPEED WIND TUNNEL; RESEARCH METHODOLOGIES; STATIC AND DYNAMIC; STATIC DERIVATIVE; SUSPENSION SYSTEM; THEORETICAL ASPECTS; WIRE-DRIVEN;

AERODYNAMICS; AIRCRAFT; ELECTRIC LOAD SHEDDING; EXPERIMENTS; SUSPENSIONS (FLUIDS); TUNNELS; WIND TUNNELS; WIRE;

SUSPENSIONS (COMPONENTS);

EID: 70249089725     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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