Energy thickness in prediction of throat heat transfer in rocket nozzles using nozzle geometries and temperature ratios.

A review of a comprehensive experimental investigation of the heat transfer and boundary layer in 30 deg to 15 deg and 60 deg to 15 deg conical nozzles is prese

An empirical modification of an existing integral energy turbulent boundary layer method is proposed in order to improve the estimates of local heat transfer in

Heat transfer in convergent-divergent nozzles with different values of wall roughness.