Dynamitic control and measurement method

The invention provides a dynamitic control and measurement method which is used for a wind tunnel test. An attack angle and a control plane deflection angle of an airplane model supported in a wind tunnel by a controllable support system are measured from flat flight to pull-up to overload G. Accord...

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Bibliographische Detailangaben
1. Verfasser: LI XINGZUO
Format: Patent
Sprache:eng
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