Development of soft x-ray multilayer mirrors for a wavelength of 3 nm [3767-34]
Computation of Supersonic Turbulent Flowfield with Secondary Jet normal to Freestream
Numerical Investigation on Transition of Shock Induced Boundary Layer
Global Strength Analysis of Wave Piercing Catamarans
Wavelength-Multiplexed Holographic Recording in Ce-SBN by Using Tunable LD
Numerical Simulation of Shock-Induced Boundary Layers in Gaps AIAA Paper
An evaluation method on LES solutions of vehicle underbody flow fields
Development of a New Generation V6 Engine Corresponding to CVT
Oxygen Storage Capacity on Cerium Oxide - Precious Metal System
Development of Plug-In Hybrid System for Midsize Car
Autonomous Precision Orbit Control for Earth-Referenced Flight Path Repeat (AAS 11-585)
Vehicle Stability Control in Limit Cornering by Active Braking
Experimental studies on methane fueled ram combustor for super/hypersonic transport
Experimental Studies on Methane Fueled Ram Combustor for Super/Hypersonic Transport
Experimental Study on Fire Protection of a WPC Car Ferry
Technical Findings of HTV Propulsion System Associated with Its Dynamic Characteristics (AAS 12-568)
Design and construction of terminal joint in the Tama River and Kawasaki Fairway tunnels
Dynamic positioned semi-submersible platform motion with riser in ultra deep water
Vehicle Stability Control in Limit Cornering by Active Brake
A Wavelength-Tunable Duplex Integrated Light Source for Fast Wavelength Switching
An Assessment of Scale-Adaptive Simulation Model on the Flow Field around a Vehicle
Development of Plug-in Hybrid System for Passenger car
Surface profile measurement of specular objects by grating projection method [4567-11]
2005-01-1385 Development of Air-Cooled Cylinder by Utilizing Natural Convection
Numerical Study of Detonation Interaction with a Single-Stage Axial Turbine
Improvement of Cylinder Cooling in Air-Cooled Engines by Utilizing Baffle Plates
Aerodynamic Effect of Turbine Blade Geometry in Pulse Detonation Combustor AIAA Paper
Aerodynamic Shape Design of the Vertical Landing Rocket Vehicle