Mathematical model analysis of axisymmetric nozzle performance prediction for complex system based on numerical simulation
Author:
Publisher
Springer Science and Business Media LLC
Subject
Strategy and Management,Safety, Risk, Reliability and Quality
Link
https://link.springer.com/content/pdf/10.1007/s13198-021-01117-8.pdf
Reference38 articles.
1. Alexeenko AA, Levin DA, Gimelshein SF, Collins RJ, Reed BD (2002) Numerical modeling of axisymmetric and three dimensional flows in microelectromechanical systems nozzles. AIAA J 40(5):897–904
2. Anderson JD (2003) Modern compressible flow. Tata McGraw-Hill Education
3. Arora R, Vaidyanathan A (2015) Experimental investigation of flow through planar double divergent nozzles. Acta Astronaut 112:200–216
4. Chouicha R, Sellam M, Bergheul S (2020) Effect of reacting gas on the fluidic thrust vectoring of an axisymmetric nozzle. Propuls Power Res. https://doi.org/10.1016/j.jppr.2020.04.002
5. Dadone A, Grossman B (2003) Fast convergence of inviscid fluid dynamic design problems. Comput Fluids 32(4):607–627
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