Internal Conical Flow about Unyawed Cones at High Speeds
Keywords: Shock wave, Hypersonic flow
AbstractAn approximate closed form solution to the internal conical, hypersonic flow about a circular cone at zero angle of incidence, has been obtained based on assumption that dissociation, and ionization etc. do not occur behind the shock wave. It has been shown that a singular line exists beyond which the solution is not valid.
How to Cite
Nath, G. (2014). Internal Conical Flow about Unyawed Cones at High Speeds. Defence Science Journal, 22(1), 1-4. https://doi.org/10.14429/dsj.22.6295
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