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Аэрогазодинамика реактивных сопел Монография

The monographs summarizes the results of fifty years investigations in Russia and abroad within the scope of aerogasdynamics of jet nozzles. Characteristics of the axisymmetric two-dimensional and three-dimensional nozzles are reported. The schemes of the nozzles are included: convergent-divergent e...

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Главный автор: Лаврухин Г.Н
Формат: Монография
Online-ссылка:https://znanium.com/catalog/document?id=218757
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200 1 |a Аэрогазодинамика реактивных сопел  |e Монография  |f Физматлит РАН 
210 1 |a Москва  |c Издательская фирма "Физико-математическая литература" (ФИЗМАТЛИТ)  |d 2003 
215 |a 375 с. 
330 |a The monographs summarizes the results of fifty years investigations in Russia and abroad within the scope of aerogasdynamics of jet nozzles. Characteristics of the axisymmetric two-dimensional and three-dimensional nozzles are reported. The schemes of the nozzles are included: convergent-divergent ejector ramp one-contour and twocontour (turbojet and turbofan) nozzles nozzles of hypersonic aircrafts and others. Characteristics of the nozzles with vector thrust; reversal thrust and nozzle suppressors are reported too. The monograph presents the generalization of the wide range of basic problems of viscous subsonic and supersonic jets in ducts and tasks about outflow of jets to a submerged space. On the base of fundamental investigations performed and features discovered the paper shows the efficiency of advanced schemes of exhaust systems their advantages and possible defects. It permits to use the data of the monograph for development of exhaust systems of the modern aircraft. The book is intended for aviation scientists postgraduates and students. 
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