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National Aerospace Laboratory | 論文
- Metallothionein induced in Amphibia (Regular Presentations) (Proceedings of the 9th Symposium on Environmental Pollutants and Toxicology)
- A High-Precision Numerical Method for the Incompressible Navier-Stokes Equations Tested by Stuart Solution
- THE RELATIONSHIP BETWEEN DISTRIBUTION OF BRYOPHYTES AND SOIL CONDITIONS ON DEGLACIATED ARCTIC TERRAIN IN NY-ÅLESUND (17th Symposium on Polar Biology)
- 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
- An Experimental Study on the Boundary Layer Transition due to Gas Injection from Capsule-shape Body Surface
- AIRCRAFT GAS TURBINES IN JAPAN(Activities in the Field of Gas Turbines and Turbochargers of JAPAN)
- OS-503 Research of Mach 5 Ramjet Propulsion System(Organized Session 5: HYPR-HST/SST Propulsion System)
- Meteorological Data Measured at Biological Hut, the Yukidori Valley, Langhovde, Antarctica in the Austral Summer of 1987-1988 and 1988-1989
- Microclimate data measured at biological hut, the Yukidori Valley, Langhovde, Antarctica in the austral summer of 1987-1988 and 1988-1989(Terrestrial Biology 3)
- Statistics of Lateral Velocity Increment in Isotropic Tubulence
- Comprehensive Study on Tip Vortex with Lateral Jet Flow
- Stress Singularity Analysis of Axisymmetric Piezoelectric Bonded Structure(Fracture Mechanics)
- Multi-Instability Analysis of Swept-Wing Boundary Layers Part2. Effects of Wall Curvature and Nonparallelism on the e^N Method
- Multi-Instability Analysis of Swept-Wing Boundary Layers Part1. A Nonparallel Model of Stability Equations
- Advected Scalar Version of the Differences between the True Dissipation and Its One-Dimensional Surrogate in Isotropic Turbulence
- On-Engine Testing of a Variable Geometry Lean-Premixed Combustor
- 2. A Torsional Strength Analysis on the Container Ship by Means of the Finite Element Procedure and Full-Scale Testing
- Visualization of the Leading-edge Vortices on a Delta Wing by using Pressure-sensitive Paint
- Comprehensive Study on Tip Vortex with Lateral Jet Flow