Computational investigation of mixing and thrust characteristics of Mach 1.64 jets issuing from contoured and straight CD nozzles
The present study investigates the mixing and thrust characteristics of Mach 1.64 jets issuing from a contoured (De Laval) nozzle and a straight convergent-divergent nozzle under overexpanded, correctly expanded, and underexpanded operating conditions. Computational simulations were performed using the SST k – ω...