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