Aero-elastic Analysis of High Aspect Ratio UAV Wing—Based on Two-Way Fluid Structure Interaction

Aero-elastic Analysis of High Aspect Ratio UAV Wing—Based on Two-Way Fluid Structure Interaction

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Veröffentlicht in:Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (8. : 2018 : Bengaluru) Design and development of aerospace vehicles and propulsion systems
1. Verfasser: Sharma, Vidit (VerfasserIn)
Weitere Verfasser: Kumar, S. Keshava (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2021
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