Investigation of aerodynamic coefficients at Mach 6 over conical, hemispherical and flat-face spiked body

Publisher: Cambridge University Press

E-ISSN: 2059-6464|121|1245|1711-1732

ISSN: 0001-9240

Source: The Aeronautical Journal, Vol.121, Iss.1245, 2017-11, pp. : 1711-1732

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Abstract