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

Assessment of Solution of the Boundary Layer Equations and Approximate Relations for Aeroheating of Axisymmetric Reentry Vehicles

R. Kamali –Moghadam; S. Nouri; M. R. Salimi; M. Sheida; S. A. Hosseini

Volume 6, Issue 3 , October 2013, , Pages 39-48

Abstract
  When a solver is used for analyzing the hypersonic reentry vehicles, high speed and accuracy of the solver results are the basic parameters in the design process. In the present study, the results obtained by solution of laminar boundary layer equations using integral matrix method and approximate method ...  Read More