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Hideaki Ogawa
Hideaki Ogawa
Verified email at aero.kyushu-u.ac.jp
Title
Cited by
Cited by
Year
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
1092008
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
1092008
SBLI control for wings and inlets
H Babinsky, H Ogawa
Shock Waves 18 (2), 89-96, 2008
832008
SBLI Control for Wings and Inlets
H Babinsky, H Ogawa
26th International Symposium on Shock Waves, 2007
832007
Inlet starting of high-contraction axisymmetric scramjets
H Ogawa, AL Grainger, RR Boyce
Journal of Propulsion and Power 26 (6), 1247-1258, 2010
582010
Inlet starting of high-contraction axisymmetric scramjets
H Ogawa, AL Grainger, RR Boyce
Journal of Propulsion and Power 26 (6), 1247-1258, 2010
582010
Physical insight into scramjet inlet behavior via multi-objective design optimization
H Ogawa, RR Boyce
AIAA journal 50 (8), 1773-1783, 2012
522012
Physical Insight into Scramjet Inlet Behaviour via Multi-Objective Design Optimisation
H Ogawa, RR Boyce
27th International Congress of The Aeronautical Sciences, 2010
522010
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
512011
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
412012
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
402016
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
402015
Wind-tunnel setup for investigations of normal shock wave/boundary layer interaction control
H Ogawa, H Babinsky
AIAA journal 44 (11), 2803-2805, 2006
322006
Evaluation of wave drag reduction by flow control
H Ogawa, H Babinsky
Aerospace science and technology 10 (1), 1-8, 2006
272006
Evaluation of Wave Drag Reduction by Flow Control
H Ogawa, H Babinsky
43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005
272005
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
262020
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
262019
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
252014
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
242015
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
212013
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