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藤澤研究室
Showing the original Japanese · View translation
航空エンジンの圧縮機に起こる不安定な流れを、試験と解析で解き明かす研究室。
AboutAbout the lab
航空エンジンの圧縮機を、試験と解析で読み解く。
藤澤研究室は、
教授の
藤澤先生は、
小型化が
Key terms
- ターボ機械
- 羽根車の
回転で 空気や 水に エネルギーを 与える、 または 取り出す機械。 圧縮機やタービンなど - 数値流体解析
- 流れを
表す方 程式を コンピュータで 解き、 目に 見えない 流れの 様子を 再現する 方法 - 旋回失速
- 圧縮機の
翼の 一部で 流れがはがれ、 その 乱れが 回転方向に ぐるぐる回りながら 伝わる 現象 - ウインドミル
- エンジンが
止まったまま、 流れ込む 空気に 押されて 圧縮機の 翼が 風車のように 回される 状態
NewsLab news
View More ↗ResearchResearch themes
太田・藤澤研究室は、
*Illustrative image旋回不安定擾乱と入口の流れの乱れ
航
*Illustrative imageディフューザで起こる旋回失速
遠心圧縮機の
*Illustrative image航空用高圧遠心圧縮機の旋回失速
航
*Illustrative imageウインドミル状態の仕事と損失
ウインドミルの
MembersFaculty
太田・藤澤研究室の
- Associate Professor藤澤 信道
VoicesStudent voices
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On a 4-point scale, ● marks where students' answers fall
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What did you learn after joining?
What's the vibe, and what is the professor like?
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RelatedLabs similar to 藤澤研究室
The information on this page is compiled by the LabLog team from the lab's public information and interviews. For corrections or removal requests, please contact LabLog, not the lab.
Report an errorAbout the images
The top and research theme images are illustrative and were not taken at the lab. They are cropped from Wikimedia Commons images. Cropped CC BY-SA images are provided under the same CC BY-SA license as the original (version shown on each line).
- Top image: “CFM56 High Pressure Compressor Rotor” Nubifer / CC BY-SA 3.0 (cropped)
- 旋回不安定擾乱と
入口の 流れの 乱れ: “Compressor case from turbojet” Olivier Cleynen / CC BY-SA 3.0 (cropped) - ディフューザで
起こる 旋回失速: “Water vortex ( )” Carlos Adampol Galindo from DF, México / CC BY-SA 2.0 (cropped) - 航
空用高圧遠心圧縮機の 旋回失速: “Impeller 2” Tiia Monto / CC BY-SA 3.0 (cropped) - ウインドミル状態の
仕事と 損失: “Five windmills with low sails ( )” Maarten Heerlien from Voorschoten, The Netherlands / CC BY 2.0 (cropped) - Related lab (太田研究室): “Blades of an axial compressor rotor, Deutsches Museum” Wilfredor / CC0 (cropped)
- Related lab (宮川研究室): “Cavitating-prop” U.S. Navy / Public domain (cropped)
- Related lab (佐藤研究室): “J58 AfterburnerT” NASA / Public domain (cropped)
- Related lab (内藤研究室): “1-50 Scale Model Of The 80X120 Foot Wind Tunnel Model (NFAC) In The Test Section Of The 40X80 Wind Tunnel At Nasa Ames (A76-0635)” NASA Ames Research Center / Public domain (cropped)
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