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(American Institute of Aeronautics and Astronautics, 2012)
(843.1KB)
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(American Institute of Aeronautics and Astronautics, 2014-01-10) (909KB)
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(American Institute of Aeronautics and Astronautics, 2012) (1.2MB)
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Experimental Investigation of Three-Dimensional Flow Development by Pitching Low-Aspect-Ratio Wing (American Institute of Aeronautics and Astronautics, 2016-01-02) (1.5MB)
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(American Institute of Aeronautics and Astronautics, 2012) (1.3MB)
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(American Institute of Aeronautics and Astronautics, 2015-01-02) (563.6KB)
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(American Institute of Aeronautics and Astronautics, 2011) (1.1MB)
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Experimental Study of Governing Parameters in Pitching and Plunging Airfoil at Low Reynolds Number (2010) (6.5MB)
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(Kluwer Academic Publishers; Society for Experimental Mechanics, Inc. ; Springer Science+Business Media, 1990-09) (1MB)
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(American Institute of Aeronautics and Astronautics, 2015-01-02) (2.4MB)
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(American Institute of Aeronautics and Astronautics, 2012) (3.4MB)
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(Peer Reviewed, 2013) (639.2KB)
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(American Institute of Aeronautics and Astronautics, 2011) (19.9MB)
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(American Institute of Aeronautics and Astronautics, 2011) (1.6MB)
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(6.2MB)
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(295.6KB)
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(American Institute of Aeronautics and Astronautics, 2016-01-01) (4MB)
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(Elsevier, 1985-10) (44.4KB)
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(American Institute of Aeronautics and Astronautics, 2011) (1.9MB)
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(Elsevier, 1978-09) (482.6KB)