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Keywords = Approximate

Number of Articles: 1
Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow

S. Ghasemloo; S. Noori

Volume 7, Issue 1 , April 2014, , Pages 41-48

Abstract
  In this paper, an approximate axisymmetric method is developed which can reliably calculate fully viscous hypersonic flow over blunt-nosed bodies. In this method, a Maslen’s second-order pressure expression is used instead of the normal momentum equation. The combination of Maslen’s second-order ...  Read More