Title: 0221 In-flight wind tunnel test system of aircraft
Abstract: Flight test data is useful and helpful to study the dynamic aerodynamic characteristics of an airplane. This report shows the trial of construction of a flight test system to fly a model airplane in a wind tunnel for the purpose of getting its flight time history data. As the wind tunnel is comparatively small, it is very difficult that two ground human pilots make fly a model airplane far a certain long time without their excellent piloting technique and help of a adequate stability and control augmentation system (SCAS).
Publication Year: 2007
Publication Date: 2007-01-01
Language: en
Type: article
Indexed In: ['crossref']
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