| Title |
-
ja
反転ファンターボジェットエンジンの研究
-
en
Study of Counter Rotating Axial Fan Turbojet Engine
|
| Creator |
-
-
ja
湊, 亮二郎
ja-Kana
ミナト, リョウジロウ
en
MINATO, Ryojiro
-
-
ja
竹田, 広人
en
TAKEDA, Hirohito
ja-Kana
タケダ, ヒロヒト
-
-
ja
西村, 宗真
en
NISHIMURA, Munemasa
ja-Kana
ニシムラ, ムネマサ
|
| Accessrights |
open access |
| Rights |
|
| Subject |
-
NDC
538
-
Other
en
counter rotating fan
-
Other
en
turbojet engine
-
Other
en
supersonic unmanned plane
|
| Description |
-
Other
application/pdf
-
Abstract
en
The Counter Rotationg Axial Fan Turbojet Engine is considered as the propulsion engine for the subscale supersonic unmanned plane, because of its aerodynamic and structural advantages. In the present study, the numerical design and analysis of counter rotating fan are conducted by Streamline Curvature Method (SCM). At same time, the two staged counter rotating turbine is also numerically designed and its aerodynamic performances are evaluated by CFD. We discussed the system integration of this type of engine based on the results of the analyses of the engine elements.
-
Other
ja
特集 : 「航空宇宙機システム研究センターにおける開発研究」 (1. 小型推進エンジンプロジェクトグループ)
|
| Publisher |
ja
室蘭工業大学
|
| Date |
|
| Language |
|
| Resource Type |
departmental bulletin paper |
| Version Type |
VoR |
| Identifier |
HDL
http://hdl.handle.net/10258/423
,
URI
https://muroran-it.repo.nii.ac.jp/records/8450
|
| Relation |
-
isIdenticalTo
NAID
120001181437
|
| Journal |
-
-
PISSN
13442708
-
NCID
AA11912609
-
ja
室蘭工業大学紀要
en
Memoirs of the Muroran Institute of Technology
-
Volume Number58
Page Start3
Page End8
|
| File |
|
| Oaidate |
2023-11-24 |
