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太田研究室
Showing the original Japanese · View translation
ターボ機械の中で起こる不安定な現象を、実験と数値解析で解き明かす、流体工学の研究室。
AboutAbout the lab
ターボ機械の中の不安定な流れを解く。
太田・藤澤研究室は、
ターボ機械の
大型の
Key terms
- ターボ機械
- 羽根車を
回転させて、 流体に エネルギーを 与えたり流体から エネルギーを 取り出したりする 機械 （圧縮機やタービンなど） - 旋回失速
- 圧縮機の
中で、 流れの 一部が 乱れて 周方向に 回転しながら 広がっていく 不安定な 現象 - サージ
- 圧縮機の
中の 流れが 激しく 脈動し、 一時的に 逆流する こともある 不安定な 現象
NewsLab news
修士課程の
学生が、 日本ガスタービン学会賞 （奨励賞）を 受賞 修士課程の
学生が、 日本ガスタービン学会 学生優秀講演賞を 受賞 論文が、
令和6年度ターボ機械協会賞 （論文賞）を 受賞 修士課程の
学生が、 機械工学記念学術賞 （関賞）を 受賞 修士課程の
学生が、 日本ガスタービン学会 学生優秀講演賞を 受賞
ResearchResearch themes
太田・藤澤研では
*Illustrative image遠心圧縮機の騒音低減
過給機に
*Illustrative image軸流圧縮機の不安定現象
小型の
*Illustrative image旋回不安定擾乱の解明
航
*Illustrative image遠心圧縮機ディフューザの不安定現象
遠心圧縮機の
MembersFaculty
太田・藤澤研究室の
- Professor太田 有
- 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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RelatedLabs similar to 太田研究室
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: “Blades of an axial compressor rotor, Deutsches Museum” Wilfredor / CC0 (cropped)
- 遠心圧縮機の
騒音低減: “RF Fully Anechoic Room 2” Mihaelawojcik / CC BY 4.0 (cropped) - 軸流圧縮機の
不安定現象: “Smoke Incense AB” Andrzej Barabasz / CC BY-SA 4.0 (cropped) - 旋回不安定擾乱の
解明: “Airplane vortex edit” NASA Langley Research Center / Public domain (cropped) - 遠心圧縮機ディフューザの
不安定現象: “Egypt - Dust devil (65797)” Mannivu / CC BY-SA 4.0 (cropped) - Related lab (藤澤研究室): “CFM56 High Pressure Compressor Rotor” Nubifer / CC BY-SA 3.0 (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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