RU2011121424A - APPLICATION OF THE EJECTOR FOR STARTING A LAVAL NOZZLE UNDER THE CONDITIONS OF A SUPERSONIC FLIGHT - Google Patents

APPLICATION OF THE EJECTOR FOR STARTING A LAVAL NOZZLE UNDER THE CONDITIONS OF A SUPERSONIC FLIGHT Download PDF

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Publication number
RU2011121424A
RU2011121424A RU2011121424/06A RU2011121424A RU2011121424A RU 2011121424 A RU2011121424 A RU 2011121424A RU 2011121424/06 A RU2011121424/06 A RU 2011121424/06A RU 2011121424 A RU2011121424 A RU 2011121424A RU 2011121424 A RU2011121424 A RU 2011121424A
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RU
Russia
Prior art keywords
ejector
starting
conditions
application
laval nozzle
Prior art date
Application number
RU2011121424/06A
Other languages
Russian (ru)
Inventor
Юрий Владимирович Туник
Original Assignee
Государственное учреждение - Научно-исследовательский институт механики Московского государственного университета имени М.В. Ломоносова
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Application filed by Государственное учреждение - Научно-исследовательский институт механики Московского государственного университета имени М.В. Ломоносова filed Critical Государственное учреждение - Научно-исследовательский институт механики Московского государственного университета имени М.В. Ломоносова
Priority to RU2011121424/06A priority Critical patent/RU2011121424A/en
Publication of RU2011121424A publication Critical patent/RU2011121424A/en

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Abstract

Применение эжектора в качестве устройства для запуска конвергентно-дивергентного сопла Лаваля в условиях сверхзвукового полета с формированием сверхзвукового потока как в конвергентной (сужающейся), так и дивергентной (расширяющейся) части сопла после вытеснения поступающим сверхзвуковым потоком покоящегося в сопловом канале газа.The use of an ejector as a device for triggering a convergent-divergent Laval nozzle in a supersonic flight with the formation of a supersonic flow in both the convergent (tapering) and divergent (expanding) parts of the nozzle after being displaced by the supersonic flow of the gas at rest in the nozzle channel.

Claims (1)

Применение эжектора в качестве устройства для запуска конвергентно-дивергентного сопла Лаваля в условиях сверхзвукового полета с формированием сверхзвукового потока как в конвергентной (сужающейся), так и дивергентной (расширяющейся) части сопла после вытеснения поступающим сверхзвуковым потоком покоящегося в сопловом канале газа. The use of an ejector as a device for triggering a convergent-divergent Laval nozzle in a supersonic flight with the formation of a supersonic flow in both the convergent (tapering) and divergent (expanding) parts of the nozzle after being displaced by the supersonic flow of the gas at rest in the nozzle channel.
RU2011121424/06A 2011-05-30 2011-05-30 APPLICATION OF THE EJECTOR FOR STARTING A LAVAL NOZZLE UNDER THE CONDITIONS OF A SUPERSONIC FLIGHT RU2011121424A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011121424/06A RU2011121424A (en) 2011-05-30 2011-05-30 APPLICATION OF THE EJECTOR FOR STARTING A LAVAL NOZZLE UNDER THE CONDITIONS OF A SUPERSONIC FLIGHT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2011121424/06A RU2011121424A (en) 2011-05-30 2011-05-30 APPLICATION OF THE EJECTOR FOR STARTING A LAVAL NOZZLE UNDER THE CONDITIONS OF A SUPERSONIC FLIGHT

Publications (1)

Publication Number Publication Date
RU2011121424A true RU2011121424A (en) 2012-12-10

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011121424/06A RU2011121424A (en) 2011-05-30 2011-05-30 APPLICATION OF THE EJECTOR FOR STARTING A LAVAL NOZZLE UNDER THE CONDITIONS OF A SUPERSONIC FLIGHT

Country Status (1)

Country Link
RU (1) RU2011121424A (en)

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20121211