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 | 125 | 2008 |
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 | 125 | 2008 |
SBLI control for wings and inlets H Babinsky, H Ogawa Shock Waves 18, 89-96, 2008 | 111 | 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 |
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 |
Physical insight into scramjet inlet behavior via multi-objective design optimization H Ogawa, RR Boyce AIAA journal 50 (8), 1773-1783, 2012 | 59 | 2012 |
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 | 59 | 2011 |
Physical Insight into Scramjet Inlet Behaviour via Multi-Objective Design Optimisation H Ogawa, RR Boyce 27th International Congress of The Aeronautical Sciences, 2010 | 59 | 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 Acta Astronautica 128, 485-498, 2016 | 46 | 2016 |
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, S Mölder, R Boyce Journal of Fluid Science and Technology 8 (2), 186-199, 2013 | 27 | 2013 |
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 Aerospace science and technology 10 (1), 1-8, 2006 | 27 | 2006 |
Evaluation of Wave Drag Reduction by Flow Control H Ogawa, H Babinsky 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005 | 27 | 2005 |