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Faculty of Engineering, Oita University | 論文
- STRUCTURAL TRANSFORMATION OF SAIKOSAPONINS BY GASTRIC JUICE AND INTESTINAL FLORA
- COMBINATION EFFECTS OF SHOSAIKOTO (CHINESE TRADITIONAL MEDICINE) AND PREDNISOLONE ON THE ANTI-INFLAMMATORY ACTION
- The Screening Method of a Bifidogenic Dietary Fiber Extracted from Inedible Parts of Vegetables
- 多孔質キトサンから再生したキチンとポリビニルアルコールとのブレンドフィルムの特性
- THE EFFECT OF TEMPERATURE AND PRESSURE ON THE MICELLE FORMATION OF SURFACTANTS IN WATER-ORGANIC SOLVENT MIXTURES
- Research on Soluble Cutting Fluids for Gear Cutting : 2nd Report, The Influence of Dilution Ratio and the Effect of Synthetic Fluids
- Research on Soluble Cutting Fluids for Gear Cutting : 1st Report, The Effect of Components of Soluble Fluids and the Range of Application of the Fluids
- Thin Film Fabrication of Bi_2(Sr, Ca)_2CuO_x Phase at Temperatures between 450 and 650℃ by Plasma-Assisted Ion Beam Sputtering
- Use of finite element method for comparison of sound field diffuseness in reverberation rooms with and without absorption materials
- Q and Site Amplification Factors of Hard-Rock Region in the Kitakami Massif, Northeastern Japan
- Investigations of Transonic Ludwieg Tubes : 4th Report, Effects of Flow Mach Number in Supply Tube on Starting Process of Test Section
- Investigations of Transonic Ludwieg Tubes : Part3 Effects of Plenum Exhaust System on Starting Process of Tunnel Test Section
- Investigations of Transonic Ludwieg Tubes Part 2 Starting Process in the Case of a Downstream Valve
- Investigation of Transonic Ludwieg Tubes Part I Starting Process in the Case of an Upstream Valve
- Quasi-Steady Population Inversions of He^+ in a Freely Expanding Plasma
- Measurement of Time-and Space-Resolved Ion Temperature in a Theta-Pinch Plasma
- System for Eddy Current Nondestructive Testing Based on Digital Signal Processing and Neural Networks
- Choking Phenomena of Flows in a Shock Tube
- The Interaction of a Reflected Shock Wave with the Contact Region in a Shock Tube
- The Interaction of a Reflected Shock Wave with the Boundary Layer in a Shock Tube