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Japan Society for Aeronautical and Space Sciences | 論文
- Experimental Approach to Improve Ion Thruster Performance: Part 2 Effects of Magnetic Field
- An Accurate Semi-Lagrangian Scheme Designed for Incompressible Navier-Stokes Equations Written in Generalized Coordinates
- Numerical Analysis of the Rarefied Plume from an Arcjet Thruster: Effect of the Nozzle Exit Shape
- Numerical Simulation of a Nitorogen Arcjet Thruster
- An Attempt at Simultaneous Optimization of Aircraft Design Using GA
- Numerical Prediction of Envelope Oscillation Phenomena of Shock-Induced Combustion
- Numerical Analyses of 2-Dimensional Axisymmetric MHD Flows Satisfying Sonic Conditions in an MPD Thruster
- Assessment of CFD Estimation of Aerodynamic Characteristics of Basic Reusable Rocket Configurations
- Thermal Choking in Three-Dimensional Scramjet Engine Models
- Nonlinear and Adaptive Nonlinear Controllers for Attitude Stabilization and Tracking of a Spacecraft
- One-Diemnsional Analytical Approximate Solution of Incompressible Viscous Laminar Oscillating Pipe Flow and Its Comparison to the Exact Uchida's Solution
- Ground Effect Calculation of a Two-Dimensional Airfoil over a Wavy Surface
- Modified Power Law for Turbulent Velocity Profile in a Two-Dimensional Channel
- Study of Surface Degradation for High-Voltage Spacecraft
- Penetration and Mixing of Hydrogen Injected Normal to a 2-Dimensional Parallel Supersonic Flow
- Budgets Turbulent Kinetic Energy in an Abruptly Expanding Circular Duct
- Measurement of Hypersonic Flow Fields around a Sidewall Compression Scramjet Inlet Using Shock Tunnel Experiments
- Reliability of Structural Components under Non-Periodic Inspection and the Optimum Inspection Plan
- Off-Design State Predictions of a Commonly Configured Loop Heat Pipe
- Extended Silverstein's Correlations on Heat Pipe Heat Transport Limits