Jet vectoring using secondary Coanda synthetic jets
In recent years, studies on the fundamental principle of thrust vectoring using jets have been conducted to realize next-generation aircraft applications. Various methods for vector control of jet flow have been proposed, such as methods that achieve control via steady, continuous jets under the Coa...
Guardado en:
Autores principales: | , , , , , |
---|---|
Formato: | article |
Lenguaje: | EN |
Publicado: |
The Japan Society of Mechanical Engineers
2020
|
Materias: | |
Acceso en línea: | https://doaj.org/article/5deec79cf6a246058c8700d349f2dbb3 |
Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
id |
oai:doaj.org-article:5deec79cf6a246058c8700d349f2dbb3 |
---|---|
record_format |
dspace |
spelling |
oai:doaj.org-article:5deec79cf6a246058c8700d349f2dbb32021-11-29T06:01:25ZJet vectoring using secondary Coanda synthetic jets2187-974510.1299/mej.20-00215https://doaj.org/article/5deec79cf6a246058c8700d349f2dbb32020-09-01T00:00:00Zhttps://www.jstage.jst.go.jp/article/mej/7/5/7_20-00215/_pdf/-char/enhttps://doaj.org/toc/2187-9745In recent years, studies on the fundamental principle of thrust vectoring using jets have been conducted to realize next-generation aircraft applications. Various methods for vector control of jet flow have been proposed, such as methods that achieve control via steady, continuous jets under the Coanda effect, steady suction flows near the Coanda surface, and synthetic jets from a neighbor slot as secondary jets. However, there are no studies on the flow direction control of jets using the secondary synthetic Coanda jet. In this study, the influence of synthetic jets near a circular cylinder on the flow characteristics of a primary jet was experimentally investigated. The main results obtained in the study were that the direction of the primary jet flow can be controlled using the secondary synthetic jet, and the degree of jet deflection depends on the frequency of the velocity oscillation for the secondary synthetic jet under an identical momentum ratio. Furthermore, when using the synthetic jet as the secondary flow, a controllable region larger than that obtained when using a steady and continuous injection or suction flow is expected. This is because secondary flow is generated using the ratio of the momentum between the primary jet and the secondary flow at the slot exit in conjunction with the dimensionless frequency of the synthetic jet based on the velocity of the primary flow at the slot exit.Ryota KOBAYASHIYuki WATANABEYu TAMANOIKoichi NISHIBEDonghyuk KANGKotaro SATOThe Japan Society of Mechanical Engineersarticlejet vectoringcoanda effectsynthetic jetfrequencycentrifugal forceMechanical engineering and machineryTJ1-1570ENMechanical Engineering Journal, Vol 7, Iss 5, Pp 20-00215-20-00215 (2020) |
institution |
DOAJ |
collection |
DOAJ |
language |
EN |
topic |
jet vectoring coanda effect synthetic jet frequency centrifugal force Mechanical engineering and machinery TJ1-1570 |
spellingShingle |
jet vectoring coanda effect synthetic jet frequency centrifugal force Mechanical engineering and machinery TJ1-1570 Ryota KOBAYASHI Yuki WATANABE Yu TAMANOI Koichi NISHIBE Donghyuk KANG Kotaro SATO Jet vectoring using secondary Coanda synthetic jets |
description |
In recent years, studies on the fundamental principle of thrust vectoring using jets have been conducted to realize next-generation aircraft applications. Various methods for vector control of jet flow have been proposed, such as methods that achieve control via steady, continuous jets under the Coanda effect, steady suction flows near the Coanda surface, and synthetic jets from a neighbor slot as secondary jets. However, there are no studies on the flow direction control of jets using the secondary synthetic Coanda jet. In this study, the influence of synthetic jets near a circular cylinder on the flow characteristics of a primary jet was experimentally investigated. The main results obtained in the study were that the direction of the primary jet flow can be controlled using the secondary synthetic jet, and the degree of jet deflection depends on the frequency of the velocity oscillation for the secondary synthetic jet under an identical momentum ratio. Furthermore, when using the synthetic jet as the secondary flow, a controllable region larger than that obtained when using a steady and continuous injection or suction flow is expected. This is because secondary flow is generated using the ratio of the momentum between the primary jet and the secondary flow at the slot exit in conjunction with the dimensionless frequency of the synthetic jet based on the velocity of the primary flow at the slot exit. |
format |
article |
author |
Ryota KOBAYASHI Yuki WATANABE Yu TAMANOI Koichi NISHIBE Donghyuk KANG Kotaro SATO |
author_facet |
Ryota KOBAYASHI Yuki WATANABE Yu TAMANOI Koichi NISHIBE Donghyuk KANG Kotaro SATO |
author_sort |
Ryota KOBAYASHI |
title |
Jet vectoring using secondary Coanda synthetic jets |
title_short |
Jet vectoring using secondary Coanda synthetic jets |
title_full |
Jet vectoring using secondary Coanda synthetic jets |
title_fullStr |
Jet vectoring using secondary Coanda synthetic jets |
title_full_unstemmed |
Jet vectoring using secondary Coanda synthetic jets |
title_sort |
jet vectoring using secondary coanda synthetic jets |
publisher |
The Japan Society of Mechanical Engineers |
publishDate |
2020 |
url |
https://doaj.org/article/5deec79cf6a246058c8700d349f2dbb3 |
work_keys_str_mv |
AT ryotakobayashi jetvectoringusingsecondarycoandasyntheticjets AT yukiwatanabe jetvectoringusingsecondarycoandasyntheticjets AT yutamanoi jetvectoringusingsecondarycoandasyntheticjets AT koichinishibe jetvectoringusingsecondarycoandasyntheticjets AT donghyukkang jetvectoringusingsecondarycoandasyntheticjets AT kotarosato jetvectoringusingsecondarycoandasyntheticjets |
_version_ |
1718407586523381760 |