詳細反応機構-燃焼LESによるロケットエンジン燃焼振動現象解明と支配噴射因子特定

• Project/Area Number: 25K01413
• Research Category: Grant-in-Aid for Scientific Research (B)
• Allocation Type: Multi-year Fund
• Section: 一般
• Review Section: Basic Section 24010:Aerospace engineering-related
• Research Institution: Hokkaido University
• Principal Investigator: 寺島 洋史 (石原 洋史) 北海道大学, 工学研究院, 准教授 (20415235)
• Project Period (FY): 2025-04-01 – 2029-03-31
• Project Status: Adopted (Fiscal Year 2025)
• Budget Amount: ¥18,460,000 (Direct Cost: ¥14,200,000、Indirect Cost: ¥4,260,000); Fiscal Year 2028: ¥4,420,000 (Direct Cost: ¥3,400,000、Indirect Cost: ¥1,020,000); Fiscal Year 2027: ¥4,680,000 (Direct Cost: ¥3,600,000、Indirect Cost: ¥1,080,000); Fiscal Year 2026: ¥3,770,000 (Direct Cost: ¥2,900,000、Indirect Cost: ¥870,000); Fiscal Year 2025: ¥5,590,000 (Direct Cost: ¥4,300,000、Indirect Cost: ¥1,290,000)