Investigation of force and thermal loading of jet deflectors of launch complexes of space rockets during the work of water supply systems
Автор: Sinilshchikov B.E., Sinilshchikov V.B.
Журнал: Космические аппараты и технологии.
Рубрика: Ракетно-космическая техника
Статья в выпуске: 2 (20), 2017 года.
Бесплатный доступ
In the most of modern launch complexes of space rockets the water supply systems are used to defend the surfaces acted directly upon by high-temperature jet flows from melting. The paper presents the estimation for parameters of force and heat loads of jet deflector during the work of intra-jet and extrajet water supply systems. The method of numerical simulation for two-phase gas-droplet flows is used. The description of a mathematical model is given. For description of gas flow the Navier-Stokes equations completed with an algebraic model of turbulence are applied, this model being similar to the Prandtl one but taking into account the influence of a droplet phase. Thermodynamic parameters are determined by the model of ideal gas for a mechanical mixture of three components: combustion products, atmospheric air, and vapor (steam) formed as a result of water evaporation. The flow of a droplet phase is calculated on the base of continual approach with using the elements of trajectory approach...
Rocket engine, jet, water supply, heat flows, evaporation, jet deflector, breakup
Короткий адрес: https://sciup.org/14117393
IDR: 14117393