Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer

Sohayla Abdolahi; Fskhri Etemadi; Mohammad Ebrahimi

Volume 8, Issue 3 , October 2015, , Pages 41-53

Abstract
  In this study, the aerodynamic heating of the flying body during powered flight phase has been numerically investigated. The conjugate simulation of fluid heat transfer and solid heat conduction has been considered. To this aim, the coupling boundary condition has been used for body shell that allows ...  Read More

Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow

S. A. Hosseini; S. Noori

Volume 7, Issue 1 , April 2014, , Pages 33-40

Abstract
  In the present work, an engineering method is developed to predict laminar and turbulent heating-rate solutions for blunt reentry spacecraft at hypersonic conditions. The calculation of aerodynamic heating around blunt bodies requires alternative solution of inviscid flow field around the hypersonic ...  Read More

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