Calculation of the three-dimensional flow field in supersonic inlets at angle of attack using a bicharacteristic method with discrete shock wave fitting
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2005 ◽
Vol 71
(701)
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pp. 154-161
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1997 ◽
Vol 4
(1)
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pp. 51-57
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2011 ◽
Vol 332-334
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pp. 260-263
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