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(American Institute of Aeronautics and Astronautics, 2017)
(3.1MB)
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(American Institute of Aeronautics and Astronautics, 2011) (560.5KB)
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(American Institute of Aeronautics and Astronautics, 2011) (1.4MB)
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(American Institute of Aeronautics and Astronautics, 2016) (1.2MB)
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(American Institute of Aeronautics and Astronautics, 2016-06-10) (1.1MB)
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(Institute of Electrical and Electronics Engineers, 2023-03) (6MB)
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(American Institute of Aeronautics and Astronautics, 2011) (1.3MB)
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(American Institute of Aeronautics and Astronautics, 2014-01-22) (1.6MB)
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(American Institute of Aeronautics and Astronautics, 2011) (4.3MB)
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(American Institute of Aeronautics and Astronautics, 2014-08-12) (4.5MB)
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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)