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Department of Aeronautics and Astronautics, Kyushu University | 論文
- D315 A NOVEL FLUIDIC MICROMOTOR DRIVEN BY THERMOCAPILLARY FORCE(Micro-scale phenomena)
- Enhanced Interlayer Coupling and Magnetoresistance Ratio in Fe_3Si/FeSi_2 Superlattices
- Low-Temperature Growth of Nanocrystalline Diamond by Reactive Pulsed Laser Deposition under a Hydrogen Atmosphere
- STUDY OF LOW-COST ORBIT DETERMINATION SYSTEM FOR TETHERED SATELLITES
- High-Velocity Carbon Plume Generated by Nd:YAG Laser for Thin Carbon Film Deposition
- Supersonic O_2-jet Impingement on Liquid Iron with Surface Chemistry
- Application of a 20kW Arc-Heated Wind Tunnel to Evaluation Tests of Wall Catalysis
- 地球低軌道における軌道環境の安定性について
- Analytical Fourier Transform of Fraunhofer Hologram Pattern of a Wire
- New Method of Tracing Interior Projectile Motion in a Gas Gun by Inline Holographic Velocimetry
- Aerodynamic Study and Mechanization Concepts for Flapping-Wing Micro Aerial Vehicles
- Implementation of Robust Stability Augmentation Systems for a Blimp
- Microheater-Driven Dancing Microbubble
- On-orbit Cryogenic Fluid Transfer Technique Using Swirl Flow Combined with Condensation by Spray Cooling : Preliminary Study of Microgravity Experiment and Thermal Analysis in Refilling Process
- TED-AJ03-361 EXPERIMENTAL STUDY ON CRYOGENIC FLOW BOILING UNDER LOW GRAVITY
- Simple Method of Calculating Gruneisen Parameter Based on the Shock Hugoniot Data for Solids
- Biological activity of extracts from Cupressus lusitanica cell culture
- Prediction of C-J state for high explosive based on the initial density dependence of detonation velocity
- Unreacted Shock Compression Curve of Energetic Materials and Modeling of Detonation and Reaction Process
- DSMC-PIC Analysis of a Plume from MUSES-C Ion Engines