| Shock-wave/boundary-layer interaction control using three-dimensional bumps for transonic wings H Ogawa, H Babinsky, M Pätzold, T Lutz AIAA journal 46 (6), 1442-1452, 2008 | 126 | 2008 |
| SBLI control for wings and inlets H Babinsky, H Ogawa Shock Waves 18, 89-96, 2008 | 112 | 2008 |
| Inlet starting of high-contraction axisymmetric scramjets H Ogawa, AL Grainger, RR Boyce Journal of Propulsion and Power 26 (6), 1247-1258, 2010 | 68 | 2010 |
| SCRAMSPACE: scramjet-based access-to-space systems R Boyce, S Tirtey, L Brown, M Creagh, H Ogawa 17th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2011 | 60 | 2011 |
| Physical Insight into Scramjet Inlet Behaviour via Multi-Objective Design Optimisation H Ogawa, RR Boyce 27th International Congress of The Aeronautical Sciences, 2010 | 60 | 2010 |
| Space traffic management: towards safe and unsegregated space transport operations S Hilton, R Sabatini, A Gardi, H Ogawa, P Teofilatto Progress in Aerospace Sciences 105, 98-125, 2019 | 48 | 2019 |
| Effects of injection angle and pressure on mixing performance of fuel injection via various geometries for upstream-fuel-injected scramjets H Ogawa 7th Asia-Pacific International Symposium on Aerospace Technology (APISAT 2015), 2015 | 46 | 2015 |
| Nozzle design optimization for axisymmetric scramjets by using surrogate-assisted evolutionary algorithms H Ogawa, RR Boyce Journal of Propulsion and Power 28 (6), 1324-1338, 2012 | 45 | 2012 |
| Mixing characteristics of inclined fuel injection via various geometries for upstream-fuel-injected scramjets H Ogawa Journal of Propulsion and Power 31 (6), 1551-1566, 2015 | 36 | 2015 |
| Numerical investigation of upstream cavity enhanced fuel mixing in scramjet combustors T Roos, A Pudsey, M Bricalli, H Ogawa Acta Astronautica 169, 50-65, 2020 | 33 | 2020 |
| Wind-tunnel setup for investigations of normal shock wave/boundary layer interaction control H Ogawa, H Babinsky AIAA journal 44 (11), 2803-2805, 2006 | 33 | 2006 |
| Multi-Objective Design and Trajectory Optimization of Space Transport Systems with RBCC Propulsion via Evolutionary Algorithms and Pseudospectral Methods M Kodera, H Ogawa, S Tomioka, S Ueda AIAA Science and Technology Forum and Exposition (SciTech 2014), 2014 | 27 | 2014 |
| Effects of Leading-Edge Truncation and Stunting on Drag and Efficiency of Busemann Intakes for Axisymmetric Scramjet Engines H Ogawa, RR Boyce, S Mölder 9th International Conference of Flow Dynamics, 2012 | 27 | 2012 |
| Evaluation of Wave Drag Reduction by Flow Control H Ogawa, H Babinsky 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005 | 27 | 2005 |
| Cavity enhanced jet interactions in a scramjet combustor T Roos, A Pudsey, M Bricalli, H Ogawa Acta Astronautica 157, 162-179, 2019 | 26 | 2019 |
| Fast estimation of internal flowfields in scramjet intakes via reduced-order modeling and machine learning S Brahmachary, A Bhagyarajan, H Ogawa Physics of Fluids 33 (10), 2021 | 25 | 2021 |
| Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines MJ Candon, H Ogawa Acta Astronautica 147, 281-296, 2018 | 25 | 2018 |
| Physical insight into fuel-air mixing for upstream-fuel-injected scramjets via multi-objective design optimization H Ogawa Journal of Propulsion and Power 31 (6), 1505-1523, 2015 | 25 | 2015 |
| Miniaturization perspectives of electrostatic propulsion for small spacecraft platforms SH Yeo, H Ogawa, D Kahnfeld, R Schneider Progress in Aerospace Sciences 126, 100742, 2021 | 24 | 2021 |
| Multi-point design optimization of a high-performance intake for scramjet-powered ascent flight S Brahmachary, C Fujio, H Ogawa Aerospace Science and Technology 107, 106362, 2020 | 23 | 2020 |
