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Reduced-Order Nonlinear Unsteady Aerodynamic Modeling Using a Surrogate-Based Recurrence Framework (2010)
(1.5MB)
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(Kluwer Academic Publishers; Society for Experimental Mechanics, Inc. ; Springer Science+Business Media, 1991-09) (1.4MB)
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(American Institute of Aeronautics and Astronautics, 2014-01-10) (2.2MB)
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(331.1KB) (18.3MB)
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(American Institute of Aeronautics and Astronautics, 2012) (1.4MB)
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(American Institute of Aeronautics and Astronautics, 2016-04-22) (1.9MB)
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(© Wiley, 1998) (195.5KB)
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(Elsevier, 1992-12) (722.4KB)
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(American Institute of Aeronautics and Astronautics, 2012) (702.6KB)
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(American Institute of Aeronautics and Astronautics, 2016-01-02) (26.5MB)
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(American Institute of Aeronautics and Astronautics, 2011) (492.8KB)
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(American Institute of Aeronautics and Astronautics, 2017) (6.6MB)
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(1.7MB)
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(Peer Reviewed, 2013) (1.4MB)
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(American Institute of Aeronautics and Astronautics, 2011) (2.6MB)
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(Peer Reviewed, 2013) (1.1MB)
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(Peer Reviewed, 2013) (710.3KB)
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(American Institute of Aeronautics and Astronautics, 2012) (2.4MB)
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(American Institute of Aeronautics and Astronautics, 2012) (4.8MB)
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(American Institute of Aeronautics and Astronautics, 2012) (1.1MB)