Numerical studies on four-engine rocket exhaust plume impinging on flame deflectors with afterburning

Author:

Zhou Zhi-tan,Zhao Chang-fang,Lu Chen-yu,Le Gui-gao

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference25 articles.

1. Numerical simulation of transient flows in a rocket propulsion nozzle;Lijo;Int J Heat Fluid Flow,2010

2. Numerical analysis of reactive turbulent flow in the thrust chamber of RD-108 engine rocket;Taghavi;Def Technol,2019

3. Low recurring cost, partially reusable heavy lift launch vehicle;Donahue;J Spacecraft Rockets,2008

4. Numerical investigation of twin-nozzle rocket plume phenomenology;Ebrahimi;J Propul Power,2000

5. Effect of freestream-plume interaction on launch vehicle aerodynamics coefficients with different flared aft-bodies;Desikan;Exp Therm Fluid Sci,2017

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