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焼野 研究室
Showing the original Japanese · View translation
極超音速の流れを数理・計算・実験で解き明かす研究室。
AboutAbout the lab
流れの機構の解明と制御で、次世代航空宇宙機へ。
焼野研究室は、
数理科学と
特許
世界最大級の
Key terms
- 極超
音速 - マッハ5
（音速の 5倍）を 超える 速さ - 乱流遷移
- なめらかに
そろった 層流が、 細かく 乱れた 乱流に 変わる こと - 磁力支持天秤装置
- 模型を
電磁力で 風洞内に 浮かせ、 支柱の 影響なしに 空気の 力を 測る 装置
NewsLab news
微小表面粗さに
よる 抵抗低減の 論文が、 Journal of Fluid Mechanics で オンライン公開 翼型まわりの
流れの 非線形最適外力解析の 論文が、 Journal of Fluid Mechanics で オンライン公開 機械学習を
使った 渦放出の 予測の 論文が、 Engineering Applications of Computational Fluid Mechanics で 公開 磁力支持天秤装置の
実験の 作品が、 サイエンスフォトコンテストの ファイナリストに 選出 研究員が、
第57回流体力学講演会で 最優秀賞 （流体力学部門）に 選出
ResearchResearch themes
航
*Illustrative image数値流体力学と流体物理理論
後退翼の
*Illustrative imageデータ科学とAI流体解析
渦の
*Illustrative image次世代の空力実験
模型を
*Illustrative image極限環境での熱と流れの制御
空力・熱・
MembersFaculty
焼野研究室の
- Associate Professor焼野 藍子
- Professor大林 茂
- Project Assistant Professor猪熊 建登
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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: “JAXA 1.27m Hypersonic Wind Tunnel P4223597” Kestrel / CC BY-SA 4.0 (cropped)
- 数値流体力学と
流体物理理論: “Flow-vector-heat-sink-fluid-WBG” Novel Concepts Inc / CC BY-SA 3.0 (cropped) - データ科学と
AI流体解析: “221206-F-KN521-2020” U.S. Air Force photo by Jill Pickett / Public domain (cropped) - 次世代の
空力実験: “Model in Supersonic Wind Tunnel GPN” NACA / Public domain (cropped) - 極限環境での
熱と 流れの 制御: “Space Shuttle Columbia launching” NASA / Public domain (cropped) - Related lab (深見 研究室): “CFD Orbiter Model - GPN” NASA / Public domain (cropped)
- Related lab (齋藤(勇) 研究室): “Space Shuttle Main Engine (SSME) Test Firing - GPN” NASA / Public domain (cropped)
- Related lab (永井・伊神 研究室): “Mars 2020 spacecraft thermal vacuum test PIA23263- D G2775 (cropped)” NASA / Public domain (cropped)
- Related lab (船本 研究室): “Microfluidic Reservoir” Kimbalm / CC BY-SA 4.0 (cropped)
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