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Information × Registration Number 0304U004276, 0101U001832 , R & D reports Title Calculations and experiments related to thermogasodynamical processes for rocket and space engines and industrial popup.stage_title Розробка теоретичних основ, методів і програмно методичного забезпечення для розрахунку локальних і інтегральних характеристик багатокомпонентних газових потоків в удосконалених або нових устроях Head Kovalenko Nikolaj Dmitrievich, Registration Date 29-04-2004 Organization Institute of Technical Mechanics NASU and NSAU popup.description2 Certain mechanisms for controlling the flow of propellant combustion products in chambers and nozzles of rocket engines with a controlled nozzle injection of solid propellant combustion products by using stem and curtain controls as well as with nozzle injection of liquids and gases through a movable/fixed injector are systematically analyzed. Methods of calculations are refined, and local and integrated characteristics of gas flows when interacted with сertain types of control mechanisms are calculated. Search studies met with recommendations related to developments of new control diagrams for supersonic gas flows in advanced engines of launcher transtages. Product Description popup.authors popup.nrat_date 2020-04-02 Close