|
ИСТИНА |
Войти в систему Регистрация |
ИПМех РАН |
||
The problem of constructing the optimal configuration of shock and detonation wavesстатья Научно-популярная статья
Дата последнего поиска статьи во внешних источниках: 19 сентября 2015 г.
- Авторы: Uskov V.N., Bulat P.V.
- Журнал: Life Science Journal
- Том: 11
- Номер: 8s
- Год издания: 2014
- Издательство: Marsland Press
- Местоположение издательства: United States
- Первая страница: 311
- Последняя страница: 314
- Аннотация: Development of technology has come to the point where new thermodynamic cycles shall be implemented in jet engines. The most promising is the thermodynamic cycle of detonation (rapid combustion). Basic concepts of shock-wave and detonation structures concepts are considered, as well as differential conditions of dynamic compatibility on shock and detonation waves. The concept of optimal shock wave and detonation structure are introduced. The task of organizing detonation combustion in preliminary generated optimal shock-wave structure is described. Basic concepts of shock adiabatic curve are given, as well as Hugoniot curve, Michelson straight lines and the model of detonation combustion of Chapman-Jouget. The concept of over-compressed and under-compressed detonation is given. Their potential application in aerospace engines is described. Formulation of task assignment of studying of structural stability of optimal shock wave and detonation structures is described. The links are provided to apply the developed mathematical tool to study the dynamics of triple configurations of shock waves in supersonic jet flows.
- Добавил в систему: Булат Павел Викторович
Прикрепленные файлы
| № | Имя | Описание | Имя файла | Размер | Добавлен |
|---|---|---|---|---|---|
| 1. | Полный текст | The_problem_of_constructing_the_optimal_configuration_of_sh… | 307,1 КБ | 30 апреля 2015 [Kulon] |