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Подвод теплоты в Ñ‚ÐµÐ¿Ð»Ð¾Ð²Ñ‹Ñ Ð³Ð°Ð·Ð¾Ð²Ñ‹Ñ Ð¼Ð°ÑˆÐ¸Ð½Ð°Ñ

учебное пособие

Подвод теплоты в Ñ‚ÐµÐ¿Ð»Ð¾Ð²Ñ‹Ñ Ð³Ð°Ð·Ð¾Ð²Ñ‹Ñ Ð¼Ð°ÑˆÐ¸Ð½Ð°Ñ

Abstract

Ð’ пособии представлен Ð¼ÐµÑ Ð°Ð½Ð¸Ð·Ð¼ эффективного преобразования природной теплоты в полную энергию потока газа в камере сгорания тепловой машины в Ñ†ÐµÐ»ÑÑ Ð¿Ñ€ÐµÐ²Ñ€Ð°Ñ‰ÐµÐ½Ð¸Ñ этой энергии в работу расширения газа и получения Ð¼ÐµÑ Ð°Ð½Ð¸Ñ‡ÐµÑÐºÐ¾Ð¹ работы. Создана теория Ñ‚ÐµÐ¿Ð»Ð¾Ð¼Ð°ÑÑÐ¾Ð¾Ð±Ð¼ÐµÐ½Ð½Ñ‹Ñ Ð¿Ñ€Ð¾Ñ†ÐµÑÑÐ¾Ð². Даны методы расчета турбулентности потока, неравномерности и нестабильности полей температуры газа за камерой сгорания. Создан метод расчета Ð½ÐµÑÑ‚Ð°Ñ†Ð¸Ð¾Ð½Ð°Ñ€Ð½Ñ‹Ñ Ð¿Ñ€Ð¾Ñ†ÐµÑÑÐ¾Ð² в камере сгорания. Разработаны методики расчетов оптимальной геометрии проточной части камеры сгорания и ее Ñ Ð°Ñ€Ð°ÐºÑ‚ÐµÑ€Ð¸ÑÑ‚Ð¸Ðº. Обоснована Ð½ÐµÐ¾Ð±Ñ Ð¾Ð´Ð¸Ð¼Ð¾ÑÑ‚ÑŒ согласования совместной работы компрессора, камеры сгорания и турбины. Приведен расчет стабилизации ударной волны подведенной за ней теплотой в Ñ†ÐµÐ»ÑÑ Ð¿Ñ€ÐµÐ¾Ð±Ñ€Ð°Ð·Ð¾Ð²Ð°Ð½Ð¸Ñ в тепловой машине энергии детонационной волны. Пособие рассчитано на студентов и специалистов, Ð·Ð°Ð½Ð¸Ð¼Ð°ÑŽÑ‰Ð¸Ñ ÑÑ проектированием и эксплуатацией Ñ‚ÐµÐ¿Ð»Ð¾Ð²Ñ‹Ñ Ð³Ð°Ð·Ð¾Ð²Ñ‹Ñ Ð¼Ð°ÑˆÐ¸Ð½.

The authors present the mechanism of effective conversion of natural heat into the full energy of gas flow in the combustion chamber of the heat engine in order to turn this energy into the work of gas expansion and obtaining mechanical work. The authors created the theory of heat-mass exchange processes, provided methods for calculating the turbulence of the flow, non-uniformity, and instability of the gas temperature fields behind the combustion chamber. The manual presents the method for calculating non-stationary processes in the combustion chamber, and methods developed for calculating the optimal geometry of the flow channel of the combustion chamber and its characteristics. The necessity of coordination of joint work of compressor, combustion chamber, and turbine is justified. The authors come up with the calculation of shock wave stabilization by the heat supplied behind it for the purpose of detonation wave energy transformation in a heat engine. The manual is intended for students and specialists involved in design and operation of heat gas engines.

Keywords

Теплота, Тепловые двигатели, Двигатели внутреннего сгорания

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citations
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
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