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(American Institute of Aeronautics and Astronautics, 2017)
(2.9MB)
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(American Institute of Aeronautics and Astronautics, 2017) (2.5MB)
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(American Institute of Aeronautics and Astronautics, 2017) (2MB)
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(American Institute of Aeronautics and Astronautics, 2016-01-02) (858.7KB)
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Understanding the effect of cube size on the near wake characteristics in a turbulent boundary layer (American Institute of Aeronautics and Astronautics, 2017) (1.3MB)
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(Peer Reviewed, 2013) (2.4MB)
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(American Institute of Aeronautics and Astronautics, 2016-01-25) (958.3KB)
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Unsteadiness characteristics and three-dimensional leading shock structure of a Mach 2.0 shock train (American Institute of Aeronautics and Astronautics, 2017) (5.1MB)
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(American Institute of Aeronautics and Astronautics, 2015-01-02) (1MB)
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(American Institute of Aeronautics and Astronautics, 2016-01-02) (991.5KB)
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(American Institute of Aeronautics and Astronautics, 2011) (10.9MB)
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(2.7MB)
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(American Institute of Aeronautics and Astronautics, 2011) (11.2MB)
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(American Institute of Aeronautics and Astronautics, 2017) (2MB)
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(American Institute of Aeronautics and Astronautics, 2017) (2.1MB)
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(American Institute of Aeronautics and Astronautics, 2011) (2.6MB)
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(American Institute of Aeronautics and Astronautics, 2017) (2.7MB)
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(American Institute of Aeronautics and Astronautics, 2016-09-09) (1.7MB)
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(American Institute of Aeronautics and Astronautics, 2017) (541.5KB)
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(Elsevier, 1993-06) (1.3MB)
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(American Institute of Aeronautics and Astronautics, 2014-08-01) (1.8MB)
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(American Institute of Aeronautics and Astronautics, 2016-02-25) (1.2MB)
