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    Полное описание

    Лаврухин, Г. Н. Аэрогазодинамика реактивных сопел : монография / Физматлит РАН. - Москва : Издательская фирма "Физико-математическая литература" (ФИЗМАТЛИТ), 2003. - 375 с. - Текст : электронный.
    УДК
    6297
    ББК
    395
    РУБ
    24.00.00

    Рубрики:
    Транспорт

    Аннотация: 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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    Держатели документа:
    ЭБС Znanium : 127282, г. Москва, ул. Полярная, д.31В, стр.1 (Шифр в БД-источнике (ZNANIUM): RU\infra-m\znanium\bibl\851562)

    Шифр в сводном ЭК: cf07a2a4fe674d9e8fd6da25ac186678



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