STAFF PROFILE
Dr. Hideaki Ogawa
Position:
Adjunct Associate Professor
College / Portfolio:
STEM College
Phone:
+61399256042
Email:
hideaki.ogawa@rmit.edu.au
Campus:
City Campus
- Responsive Access to Space (CRC-P 5000038). Funded by: CRC-P Cooperative Research Centre Project (DefendTex) from (2018 to 2021)
- Hydrocarbon Fuel Technology for Hypersonic Air Breathing Vehicles (Administered by Defendtex, CRC-P50510). Funded by: CRC-P Cooperative Research Centre Project (DefendTex) from (2017 to 2019)
- High-Fidelity Modelling of Wing Flutter and Nonlinear Aeroelastic Predictions. Funded by: Defence Science Institute Research Higher Degree Grants 2015 from (2016 to 2018)
- Design optimisation and phsyical behaviour of fuel injection and mixing for innovative scramjet concepts. Funded by: ARC Discovery Early Career Researcher from (2012 to 2018)
4 PhD Completions and 1 Masters by Research Completions
High-speed aerodynamics, Multi-objective design optimisation, Supersonic/hypersonic vehicle design, Space transport, Propulsion, Computational fluid dynamics, Evolutionary algorithms, Shock/boundary--layer interactions, Flow control
- Candon, M.,Levinski, O.,Ogawa, H.,Carrese, R.,Marzocca, P. (2022). A nonlinear signal processing framework for rapid identification and diagnosis of structural freeplay In: Mechanical Systems and Signal Processing, 163, 1 - 29
- Roos, T.,Pudsey, A.,Ogawa, H. (2021). Numerical investigation of combustion characteristics of upstream crescent cavities in a scramjet combustor In: Acta Astronautica, 187, 43 - 60
- Yeo, S.,Ogawa, H.,Kahnfeld, D.,Schneider, R. (2021). Miniaturization perspectives of electrostatic propulsion for small spacecraft platforms In: Progress in Aerospace Sciences, 126, 1 - 19
- Roos, T.,Pudsey, A.,Bricalli, M.,Ogawa, H. (2020). Numerical investigation of upstream cavity enhanced fuel mixing in scramjet combustors In: Acta Astronautica, 169, 50 - 65
- Yeo, S.,Ogawa, H.,Matthias, P.,Kahnfeld, D.,Schneider, R. (2020). Multiobjective Optimization and Particle-In-Cell Simulation of Cusped Field Thrusters for Microsatellite Platforms In: Journal of Spacecraft and Rockets, 57, 603 - 611
- Roos, T.,Pudsey, A.,Bricalli, M.,Ogawa, H. (2020). Numerical investigation of fuel mixing with upstream crescent cavities in a scramjet combustor In: Acta Astronautica, 177, 611 - 626
- Hilton, S.,Sabatini, R.,Gardi, A.,Ogawa, H.,Teofilatto, P. (2019). Space traffic management: towards safe and unsegregated space transport operations In: Progress in Aerospace Sciences, 105, 98 - 125
- Shoev, G.,Ogawa, H. (2019). Numerical study of viscous effects on centreline shock reflection in axisymmetric flow In: Physics of Fluids, 31, 1 - 13
- Ravindran, M.,Bricalli, M.,Pudsey, A.,Ogawa, H. (2019). Mixing characteristics of cracked gaseous hydrocarbon fuels in a scramjet combustor In: Acta Astronautica, 162, 168 - 184
- Matthias, P.,Kahnfeld, D.,Schneider, R.,Yeo, S.,Ogawa, H. (2019). Particle-in-cell simulation of an optimized high-efficiency multistage plasma thruster In: Contributions to Plasma Physics, , 1 - 12