NASA Technical Reports Server (NTRS) 19820003197: An influence coefficient method for the application of the modal technique to wing flutter suppression of the DAST ARW-1 wingReport as inadecuate



 NASA Technical Reports Server (NTRS) 19820003197: An influence coefficient method for the application of the modal technique to wing flutter suppression of the DAST ARW-1 wing


NASA Technical Reports Server (NTRS) 19820003197: An influence coefficient method for the application of the modal technique to wing flutter suppression of the DAST ARW-1 wing - Download this document for free, or read online. Document in PDF available to download.

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The methods used to compute the mass, structural stiffness, and aerodynamic forces in the form of influence coefficient matrices as applied to a flutter analysis of the Drones for Aerodynamic and Structural Testing (DAST) Aeroelastic Research Wing. The DAST wing was chosen because wind tunnel flutter test data and zero speed vibration data of the m

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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