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TypeAuthor(s)TitleOther TitlesCitationCitation(alt)Issue Date
articleYu, Minghao; Qiu, Zeyang; Zhong, Bowen; Takahashi, YusukeNumerical simulation of thermochemical non-equilibrium flow-field characteristics around a hypersonic atmospheric reentry vehicle-Physics of fluids-8-Dec-2022
articleTakahashi, YusukePropagation Path of Radio Waves in Nonequilibrium Reentry Plasma Around a Nanosatellite With an Inflatable Aeroshell-IEEE Transactions on Aerospace and Electronic Systems-Oct-2022
articleTakahashi, Yusuke; Saito, Masahiro; Oshima, Nobuyuki; Yamada, KazuhikoTrajectory reconstruction for nanosatellite in very low Earth orbit using machine learning-Acta astronautica-May-2022
articleTakahashi, Yusuke; Takasawa, Hideto; Yamada, Kazuhiko; Shimoda, TakayukiNonequilibrium shock layer in large-scale arc-heated wind tunnel-Journal of Physics D : Applied Physics-14-Mar-2022
articleYu, Minghao; Qiu, Zeyang; Lv, Bo; Takahashi, YusukeMultiphysics Mathematical Modeling and Flow Field Analysis of an Inflatable Membrane Aeroshell in Suborbital Reentry-Mathematics-Mar-2022
article (author version)Takahashi, Yusuke; Enoki, Naoya; Koike, Taiki; Tanaka, Mayuko; Yamada, Kazuhiko; Shimoda, TakayukiFlow Enthalpy of Nonequilibrium Plasma in 1 MW Arc-Heated Wind Tunnel-AIAA Journal-Jan-2021
articleTakahashi, Yusuke; Ohashi, Tatsushi; Oshima, Nobuyuki; Nagata, Yasunori; Yamada, KazuhikoAerodynamic instability of an inflatable aeroshell in suborbital re-entry-Physics of fluids-1-Jul-2020
article (author version)Takahashi, Yusuke; Enoki, Naoya; Takasawa, Hideto; Oshima, NobuyukiSurface catalysis effects on mitigation of radio frequency blackout in orbital reentry-Journal of Physics D : Applied Physics-3-Jun-2020
article (author version)Takahashi, Yusuke; Matsunaga, Manabu; Oshima, Nobuyuki; Yamada, KazuhikoDrag Behavior of Inflatable Reentry Vehicle in Transonic Regime-Journal of Spacecraft and Rockets-Mar-2019
article (author version)Takahashi, Yusuke; Yamada, KazuhikoAerodynamic heating of inflatable aeroshell in orbital reentry-Acta astronautica-Nov-2018
article (author version)Takahashi, Yusuke; Yamada, KazuhikoAerodynamic-Heating Analysis of Sample-Return Capsule in Future Trojan-Asteroid Exploration-Journal of thermophysics and heat transfer-Jul-2018
proceedings (author version)Koike, Taiki; Takahashi, Yusuke; Oshima, Nobuyuki; Yamada, KazuhikoAerodynamic Heating Prediction of Flare-type Membrane Inflatable Reentry Vehicle from Low Earth Orbit---Jan-2018
article (author version)Takahashi, Yusuke; Esser, Burkard; Steffens, Lars; Gülhan, AliPlasma flow modeling for Huels-type arc heater with turbulent diffusion-Physics of Plasmas-Dec-2017
article (author version)Kamps, Landon; Saito, Yuji; Kawabata, Ryosuke; Wakita, Masashi; Totani, Tsuyoshi; Takahashi, Yusuke; Nagata, HarunoriMethod for Determining Nozzle-Throat-Erosion History in Hybrid Rockets-Journal of propulsion and power-Nov-2017
article (author version)Takahashi, Yusuke; Ha, Dongheun; Oshima, Nobuyuki; Yamada, Kazuhiko; Abe, Takashi; Suzuki, KojiroAerodecelerator Performance of Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry-Journal of Spacecraft and Rockets-Sep-2017
proceedings (author version)Matsunaga, Manabu; Takahashi, Yusuke; Oshima, Nobuyuki; Yamada, KazuhikoAerodynamic Heating Prediction of an Inflatable Reentry Vehicle in a Hypersonic Wind Tunnel---Jan-2017
articleTakahashi, Yusuke; Nakasato, Reo; Oshima, NobuyukiAnalysis of Radio Frequency Blackout for a Blunt-Body Capsule in Atmospheric Reentry Missions-Aerospace-6-Jan-2016
article (author version)Takahashi, YusukeAdvanced validation of CFD-FDTD combined method using highly applicable solver for reentry blackout prediction-Journal of Physics D: Applied Physics-18-Nov-2015
article (author version)Takahashi, Yusuke; Yamada, Kazuhiko; Abe, Takashi; Suzuki, KojiroAerodynamic Heating Around Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry Demonstration Flight-Journal of spacecraft and rockets-Nov-2015
article (author version)Takahashi, Yusuke; Yamada, Kazuhiko; Abe, TakashiPrediction Performance of Blackout and Plasma Attenuation in Atmospheric Reentry Demonstrator Mission-Journal of Spacecraft and Rockets-Nov-2014
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