1. Miller, D.N., Catt, J.A.: Conceptual development of fixed-geometry nozzles using fluidic injection for throat-area control. AIAA-95-2603
2. McArdle, J.G.: Internal characteristics and performance of an aerodynamically controlled, variable discharge convergent nozzle. NACA-TN4312, July 1958
3. Damiel, Y., Miller, N., Patrick, J.Y., Jeffrey, W.H.: Fluidic throat skewing for thrust vectoring in fixed-geometry nozzles. AIAA-99-0365
4. Baruzzini, D., Domel, N., Miller, D.N., et al.: Pulsed injection flow control for throttling in supersonic nozzles—a computational fluid dynamics design study. AIAA-2007-4215
5. Xie, K.: Numerical and Experimental Study on Fluid Throat of Solid Rocket Engine. Beihang University, Beijing