Method for determining rigidity of flexible airfoil suitable for distributed parabola type crankshaft driving

The invention provides a method for determining the rigidity of a flexible airfoil adapting to distributed parabolic crankshaft driving. The method comprises the following steps: setting a preset condition, and giving a known quantity; obtaining a movable trailing edge centerline parabola analytic e...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LI KANG, DENG YANGCHEN, SONG SHUFANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT AVIATION CALCULATING COMPUTING COSMONAUTICS COUNTING DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ELECTRIC DIGITAL DATA PROCESSING GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS PHYSICS TRANSPORTING
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