Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods / S. M. Aulchenko [et al .]
Уровень набора: Journal of Engineering Physics and Thermophysics, Scientific JournalЯзык: английский.Страна: .Резюме или реферат: On the basis of the solution of direct problems with the use of various medium models and numerical methods of integration of gas flow equations, methods for designing super- and hypersonic nozzles have been developed. Multimode nozzles in the ranges of Mach numbers 8-14 and 14-20 satisfying given conditions have been designed..Примечания о наличии в документе библиографии/указателя: [References: p. 1131 (8 tit.)].Аудитория: .Тематика: электронный ресурс | труды учёных ТПУ Ресурсы он-лайн:Щелкните здесь для доступа в онлайнНет реальных экземпляров для этой записи
Title screen
[References: p. 1131 (8 tit.)]
On the basis of the solution of direct problems with the use of various medium models and numerical methods of integration of gas flow equations, methods for designing super- and hypersonic nozzles have been developed. Multimode nozzles in the ranges of Mach numbers 8-14 and 14-20 satisfying given conditions have been designed.
Для данного заглавия нет комментариев.
Личный кабинет оставить комментарий.