Numerical solutions of full Navier-Stokes equations with chemical reaction flow were obtained for of the LOX/HTPB hybrid rocket motor.

• 利用二维轴对称N-S方程和组分方程对选用液氧/端羟基聚丁二烯推进剂的固液混合火箭发动机的燃烧室和喷管进行了一体化计算。