Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics

Modern aircraft need increased maneuverability to maintain a competitive position. One way to improve this characteristic is to use methods to adjust the thrust vectors of a jet engine nozzle. One method of controlling nozzle thrust is the use of nozzle interceptors devices of various shapes that e...

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Main Authors: K. O. Tishchenko, N. A. Brykov, A. S. Belyaeva
Format: Article
Language:English
Published: Samara National Research University 2022-01-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/10010/8848
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author K. O. Tishchenko
N. A. Brykov
A. S. Belyaeva
author_facet K. O. Tishchenko
N. A. Brykov
A. S. Belyaeva
author_sort K. O. Tishchenko
collection DOAJ
description Modern aircraft need increased maneuverability to maintain a competitive position. One way to improve this characteristic is to use methods to adjust the thrust vectors of a jet engine nozzle. One method of controlling nozzle thrust is the use of nozzle interceptors devices of various shapes that extend into the nozzle channel and cause an uneven distribution of pressure along the walls of the channel. The extension of the rod interceptor near the critical section of the nozzle creates a greater lateral force than the extension of the rod near the exit section. The dependence of the lateral force on the extension height is nonlinear. The article presents a description of a nozzle interceptor of a cylindrical shape extended from the channel wall. Numerical simulation of gas flow in the nozzle with a cylindrical interceptor was carried out. The patterns of gas flow in the channel and in the environment outside the nozzle are presented. The plots of the lateral and axial components of the thrust force against the interceptor rod length are also presented for both cases of the rod location. Rod interceptors can be used in combination with other correcting devices.
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spelling doaj.art-3fed705f85924d99aed5092713a071f32023-03-14T07:00:11ZengSamara National Research UniversityВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение2542-04532541-75332022-01-01204525810.18287/2541-7533-2021-20-4-52-588579Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristicsK. O. Tishchenko0N. A. Brykov1A. S. Belyaeva2Baltic State Technical University “VOENMEH” named after D.F. UstinovBaltic State Technical University “VOENMEH” named after D.F. UstinovBaltic State Technical University “VOENMEH” named after D.F. UstinovModern aircraft need increased maneuverability to maintain a competitive position. One way to improve this characteristic is to use methods to adjust the thrust vectors of a jet engine nozzle. One method of controlling nozzle thrust is the use of nozzle interceptors devices of various shapes that extend into the nozzle channel and cause an uneven distribution of pressure along the walls of the channel. The extension of the rod interceptor near the critical section of the nozzle creates a greater lateral force than the extension of the rod near the exit section. The dependence of the lateral force on the extension height is nonlinear. The article presents a description of a nozzle interceptor of a cylindrical shape extended from the channel wall. Numerical simulation of gas flow in the nozzle with a cylindrical interceptor was carried out. The patterns of gas flow in the channel and in the environment outside the nozzle are presented. The plots of the lateral and axial components of the thrust force against the interceptor rod length are also presented for both cases of the rod location. Rod interceptors can be used in combination with other correcting devices.https://journals.ssau.ru/vestnik/article/viewFile/10010/8848rocket enginenozzleinterceptor
spellingShingle K. O. Tishchenko
N. A. Brykov
A. S. Belyaeva
Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
rocket engine
nozzle
interceptor
title Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics
title_full Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics
title_fullStr Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics
title_full_unstemmed Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics
title_short Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics
title_sort parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics
topic rocket engine
nozzle
interceptor
url https://journals.ssau.ru/vestnik/article/viewFile/10010/8848
work_keys_str_mv AT kotishchenko parametricstudyoftheinfluenceoflocationandextensionheightoftherodinterceptoronjetenginenozzlecharacteristics
AT nabrykov parametricstudyoftheinfluenceoflocationandextensionheightoftherodinterceptoronjetenginenozzlecharacteristics
AT asbelyaeva parametricstudyoftheinfluenceoflocationandextensionheightoftherodinterceptoronjetenginenozzlecharacteristics