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This final qualification work is devoted to the calculation and design of a turbojet two-circuit twin-shaft aviation engine of 147 kN directional thrust based on the ÐÐ-14 prototype, a Russian 5th generation turbofan engine intended for the medium-haul narrow-body passenger aircraft ÐС-21.
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2017
Темой дипломной ÑабоÑÑ ÑвлÑеÑÑÑ Â«ÐонÑÑÑÑкÑивнÑе ÑеÑÐµÐ½Ð¸Ñ ÑÑÐµÑ ÑÑажного многокваÑÑиÑного жилого дома». ÐеÑÑо ÑÑÑоиÑелÑÑÑва г. СанкÑ-ÐеÑеÑбÑÑг, ÐÑимоÑÑкийм Ñайон, ÐÐ¾Ð½Ð½Ð¾Ð»Ð°Ñ ÑинÑкий пÑ., д. 34..
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Темой дипломной ÑабоÑÑ ÑвлÑеÑÑÑ Â«ÐонÑÑÑÑкÑивнÑе ÑеÑÐµÐ½Ð¸Ñ ÑÑÐµÑ ÑÑажного многокваÑÑиÑного жилого дома». ÐеÑÑо ÑÑÑоиÑелÑÑÑва г. СанкÑ-ÐеÑеÑбÑÑг, ÐÑимоÑÑкийм Ñайон, ÐÐ¾Ð½Ð½Ð¾Ð»Ð°Ñ ÑинÑкий пÑ., д. 34..
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