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Source: MATEC Web of conferences. 2017. Vol. 115. P. 02012 (1-4)
Type: статьи в журналах
Date: 2017
Description:
A technique of experimental determination of the parameters and structure of supersonic air flow around of axisymmetric bodies form in the range of Mach numbers M = (2 ÷ 5) are presented. The results
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Type: сборники
Date: 1987
Type: монографии
Date: 1984
Type: диссертации
Date: 1968