Technique consists of measuring response of aeroelastically scaled model in simulated free flight to gust field generated in wind tunnel by oscillating airfoils located upstream of test section; freedom of model in approximation of free flight is provided by two-cable support system; description of airstream oscillator system and model mount system; some results of application to fighter-type model are presented.
Wind-tunnel technique for measuring frequency-response functions for gust load analyses
J Aircraft
Journal of Aircraft ; 3 , n 6
1966
6 pages
Article (Journal)
English
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