Static Aeroelastic and Longitudinal Trim Model of Flexible Wing Aircraft Using Finite-Element Vortex-Lattice Coupled Solution (AIAA 2014-0837)
Conference; 55th, AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials ; 2014 ; National Harbor, MD
2014-01-01
29 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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Coupled Aeroelastic Vortex Lattice Modeling of Flexible Aircraft
British Library Conference Proceedings | 2011
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