This paper proposes a boundary layer based optimization method to improve the aerodynamic performance of the waverider under the condition of strong viscous
Prediction of aerodynamic heating under different flight conditions is a critical and challenging step in developing a new hypersonic vehicle.The prediction
An expansion tube facility is operated for producing high-enthalpy flows at the nominal velocity of 8km/s relevant to Earth reentry.A semicircle edge model
Traditional structured/unstructured mesh generation technique costs long computing time.Usually,for a two-dimensional simulation,it costs hours;for a three-