1–14 von 14 Ergebnissen
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    Behavior of Two-Temperature Model in Intermediate Hypersonic Regime

    Michiko Furudate / Satoshi Nonaka / Keisuke Sawada | AIAA | 1999

    Calculation of Radiating Flowfield Behind a Reflected Shock Wave in Air

    Takeharu Sakai / Keisuke Sawada / Chul Park | AIAA | 1999

    Application of PlanckRosselandGray Model for High-Enthalpy Arc Heaters

    Takeharu Sakai / Keisuke Sawada / Masahiko Mitsuda | AIAA | 2001

    Computation of Hypersonic Radiating Flowfield over a Blunt Body

    Takeharu Sakai / Tomoko Tsuru / Keisuke Sawada | AIAA | 2001

    Response of Heatshield Material at Stagnation Point of Pioneer-Venus Probes

    Hyo-Keun Ahn / Chul Park / Keisuke Sawada | AIAA | 2002

    Unified Calculation of Hypersonic Flowfield for a Reentry Vehicle

    Toshiyuki Suzuki / Michiko Furudate / Keisuke Sawada | AIAA | 2002

    Parallel Computation of Fully Coupled Hypersonic Radiating Flowfield Using Multiband Model

    Shingo Matsuyama / Takeharu Sakai / Akihiro Sasoh et al. | AIAA | 2003

    Calculation of Shock Shapes over Sharp Cone in Intermediate Hypersonic Airflow

    Michiko Furudate / Satoshi Nonaka / Keisuke Sawada | AIAA | 2003

    Gas Permeability of Oblique-Layered Carbon-Cloth Ablator

    Toshiyuki Suzuki / Keisuke Sawada / Tetsuya Yamada et al. | AIAA | 2004

    Numerical Simulation of Galileo Probe Entry Flowfield with Radiation and Ablation

    Shingo Matsuyama / Naofumi Ohnishi / Akihiro Sasoh et al. | AIAA | 2005

    Experimental and Numerical Study of Pyrolysis Gas Pressure in Ablating Test Piece

    Toshiyuki Suzuki / Keisuke Sawada / Tetsuya Yamada et al. | AIAA | 2005

    Multiband Radiation Model for Simulation of Galileo Probe Entry Flowfield

    Shingo Matsuyama / Yuji Shimogonya / Naofumi Ohnishi et al. | AIAA | 2006