





Journal Articles (31)

Candon, M, Carrese, R, Ogawa, H, Marzocca, P, Mouser, C and Levinski, O 2019, 'Characterization of a 3DOF aeroelastic system with freeplay and aerodynamic nonlinearities  Part II: HilbertHuang transform', Mechanical Systems and Signal Processing, vol. 14, pp. 628643.

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Klink, P and Ogawa, H 2019, 'Investigation on the performance and feasibility of RBCCbased accesstospace via multiobjective design optimization', Acta Astronautica, vol. 157, pp. 435454.

7 




Ravindran, M, Bricalli, M, Pudsey, A and Ogawa, H 2019, 'Mixing characteristics of cracked gaseous hydrocarbon fuels in a scramjet combustor', Acta Astronautica, vol. 162, pp. 168184.

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Matthias, P, Kahnfeld, D, Schneider, R, Yeo, S and Ogawa, H 2019, 'Particleincell simulation of an optimized highefficiency multistage plasma thruster', Contributions to Plasma Physics, pp. 112.

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Hilton, S, Sabatini, R, Gardi, A, Ogawa, H and Teofilatto, P 2019, 'Space traffic management: towards safe and unsegregated space transport operations', Progress in Aerospace Sciences, vol. 105, pp. 98125.

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4

Roos, T, Pudsey, A, Bricalli, M and Ogawa, H 2019, 'Cavity enhanced jet interactions in a scramjet combustor', Acta Astronautica, vol. 157, pp. 162179.

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Shoev, G and Ogawa, H 2019, 'Numerical study of viscous effects on centreline shock reflection in axisymmetric flow', Physics of Fluids, vol. 31, no. 2, pp. 113.

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Candon, M, Carrese, R, Ogawa, H, Marzocca, P, Mouser, C, Levinski, O and Silva, W 2018, 'Characterization of a 3DOF aeroelastic system with freeplay and aerodynamic nonlinearities Part I: Higherorder spectra', Mechanical Systems and Signal Processing, vol. 118, pp. 628643.

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Candon, M and Ogawa, H 2018, 'Numerical analysis and design optimization of supersonic afterburning with strut fuel injectors for scramjet engines', Acta Astronautica, vol. 147, pp. 281296.

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Boom, Y, Lio, K and Ogawa, H 2018, 'Optimization of BackwardFacing Step Flow Control Using Dielectric Barrier Discharge Plasma Actuators', International Journal of Aeronautical and Space Sciences, vol. 19, no. 3, pp. 595605.

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Fahey, T, Muffatti, A and Ogawa, H 2017, 'High Fidelity MultiObjective Design Optimization of a Downscaled Cusped Field Thruster', Aerospace, vol. 4, no. 4, 55, pp. 120.

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Candon, M, Carrese, R, Ogawa, H and Marzocca, P 2017, 'Identification of freeplay and aerodynamic nonlinearities in a 2D aerofoil system with via higherorder spectra', Aeronautical Journal, vol. 121, no. 1244, pp. 15301560.

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Yu, S, Jones, T, Ogawa, H and Karwa, N 2017, 'Multiobjective design optimization of precoolers for hypersonic airbreathing propulsion', Journal of Thermophysics and Heat Transfer, vol. 31, no. 2, pp. 421433.

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Ogawa, H 2016, 'Effects of injection angle and pressure on mixing performance of fuel injection via various geometries for upstreamfuelinjected scramjets', Acta Astronautica, vol. 128, pp. 485498.

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Cited 3 times in Scopus3

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Candon, M, Carrese, R, Joseph, N, Ogawa, H and Marzocca, P 2016, 'Evolutionary optimization of transonic airfoils for static and dynamic trim performance', Journal of Intelligent Material Systems and Structures, vol. 27, pp. 118.

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Michael, C, Ogawa, H and Dorrington, G 2015, 'Thrust augmentation through afterburning in scramjet nozzles', Advances in aircraft and spacecraft science, vol. 2, no. 2, pp. 183198.

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Ogawa, H and Kodera, M 2015, 'Physical insight into fuel/air mixing with hypermixer injectors for scramjet engines', Journal of Propulsion and Power, vol. 31, no. 5, pp. 14231435.

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Michael, C and Ogawa, H 2015, 'Thrust augmentation optimization through supersonic afterburning in scramjet engine nozzles via surrogateassisted evolutionary algorithms', Acta Astronautica, vol. 116, pp. 132147.

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Cited 2 times in Scopus2

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Ogawa, H 2015, 'Physical insight into fuelair mixing for upstreamfuelinjected scramjets via multiobjective design optimization', Journal of Propulsion and Power: devoted to aerospace propulsion and power, vol. 31, no. 5, pp. 15051523.

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Cited 4 times in Scopus4

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Ogawa, H 2015, 'Mixing characteristics of inclined fuel injection via various geometries for upstreamfuelinjected scramjets', Journal of Propulsion and Power, vol. 31, no. 6, pp. 15511566.

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Cited 3 times in Scopus3

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Ho, T, Ogawa, H and Bil, C 2015, 'Investigation on effective sampling strategy for multiobjective design optimization of RBCC propulsion systems via surrogateassisted evolutionary algorithms', Procedia Engineering, vol. 99, pp. 12521262.

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Cited 1 times in Scopus1

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Ogawa, H and Molder, S 2014, 'Numerical analysis of hysteresis in mode transition of centerline mach reflection in stunted busemann intakes for axisymmetric scramjet engines', JAXA Special Publication, JAXASP13011, pp. 145150.

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Ogawa, H, Molder, S and Boyce, R 2013, 'Effects of leadingedge truncation and stunting on drag and efficiency of busemann intakes for axisymmetric scramjet engines', Journal of Fluid Science and Technology, vol. 8, no. 2, pp. 186199.

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Ogawa, H and Boyce, R 2012, 'Nozzle design optimization for axisymmetric scramjets by using surrogateassisted evolutionary algorithms', Journal of Propulsion and Power, vol. 28, no. 6, pp. 13241338.

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Cited 15 times in Scopus15

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Ogawa, H and Boyce, R 2012, 'Physical insight into scramjet inlet behavior via multiobjective design optimization', AIAA Journal, vol. 50, no. 8, pp. 17731783.

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Cited 19 times in Scopus19

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Ogawa, H, Boyce, R, Amitay, I and Tapabrata, R 2010, 'Multiobjective design optimisation of inlet and combustor for axisymmetric scramjets', Open Thermodynamics Journal, vol. 4, no. 6, pp. 8691.

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Ogawa, H, Grainger, A and Boyce, R 2010, 'Inlet starting of highcontraction axisymmetric scramjets', Journal of Propulsion and Power, vol. 26, no. 6, pp. 12471258.

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Cited 28 times in Scopus28

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Ogawa, H, Babinsky, H, Patzold, M and Lutz, T 2008, 'Shockwave/boundarylayer interaction control using threedimensional bumps for transonic wings', AIAA Journal, vol. 46, no. 6, pp. 14421452.

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Cited 64 times in Scopus64

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Babinsky, H and Ogawa, H 2008, 'SBLI control for wings and inlets', Shock Waves, vol. 18, no. 2, pp. 8996.

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Cited 41 times in Scopus41

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Ogawa, H and Babinsky, H 2006, 'Windtunnel setup for investigations of normal shock wave/boundary layer interaction control', AIAA Journal, vol. 44, no. 11, pp. 28032805.

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Cited 34 times in Scopus34

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Ogawa, H and Babinsky, H 2006, 'Evaluation of wave drag reduction by flow control', Aerospace Science and Technology, vol. 10, no. 1, pp. 18.

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Cited 16 times in Scopus16

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Conference Papers (20)

Klink, P, Coulloupas, G and Ogawa, H 2017, 'Performance Analysis of RBCCBased TSTO Space Transportation Systems via MultiObjective Design Optimisation', in 68th International Astronautical Congress 2017, Adelaide, Australia, 2529 September 2017, pp. 114.

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Lim, V, Ogawa, H, Coulloupas, G and Chadwick, D 2017, 'Optimising the Launch and Deployment of a Smallsat Constellation', in Proceedings of the 16th Australian Space Research Conference, Melbourne, Australia, 2628 September 2016, pp. 120.

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Muffatti, A and Ogawa, H 2017, 'Multiobjective Design Optimisation of a small scale Cusped Field Thruster for microsatellite platforms', in Proceedings of the 16th Australian Space Research Conference 2016, Melbourne, Australia, 2628 September 2016, pp. 116.

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Dorrington, G, Ogawa, H and Trivailo, P 2017, 'Enceladus Plume and Icy Body Exospheric Particle Sampling Using Rotating Tether and Alternative Architectures', in 68th International Astronautical Congress, Adelaide, Australia, 2529 September 2017, pp. 115.

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Coulloupas, G, Ogawa, H and Mo, J 2017, 'A Systems Engineering Approach to Miniaturised Satellite Constellation Design Optimisation', in Proceedings of the 16th Australian Space Research Conference 2016, Melbourne, Australia, 2628 September 2016, pp. 114.

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Tanimizu, K, Jones, T, Ogawa, H and Pudsey, A 2016, 'Numerical investigation of the flow structures in a quasiaxisymmetric scramjet engine', in Proceedings of the 20th Australasian Fluid Mechanics Conference, Perth, Australia, 58 December 2016, pp. 14.

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Shoesmith, B, Molder, S, Ogawa, H and Timofeev, E 2016, 'Shock reflection in axisymmetric internal flows', in Proceedings of the 22nd International Shock Interaction Symposium, Glasgow, United Kingdom, 48 July 2016, pp. 15.

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Candon, M, Carrese, R, Ogawa, H and Marzocca, P 2016, 'Characterization of the nonlinear aeroelastic behavior of an airfoil with freeplay and aerodynamic nonlinearity', in Proceedings of the 30th Congress of the International Council of Aeronautical Sciences (ICAS 2016), Daejeon, South Korea, 2530 September 2016, pp. 111.

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Ogawa, H, Shoesmith, B, Molder, S and Timofeev, E 2016, 'Viscous correction and shock reflection in stunted Busemann intakes', in Proceedings of the 22nd International Shock Interaction Symposium, Glasgow, United Kingom, 48 July 2016, pp. 18.

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Jones, T, Karwa, N, Ogawa, H and Rosengarten, G 2016, 'Flow analysis of the effect of tube geometry on the performance of precoolers for turbinebased hypersonic airbreathing propulsion', in 7th AsiaPacific International Symposium on Aerospace Technology (APISAT 2015), Cairns, Australia, 2527 Nov 2015, pp. 500509.

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Jayatissa, H, Berdilek, M, Bil, C and Ogawa, H 2015, 'Feasibility study of a Mach 4.0 supersonic business transport', in AIAC16: 16th Australian International Aerospace Congress, Melbourne Convention Centre, Melbourne, Australia, 2324 February 2015, pp. 256261.

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Ogawa, H, Wen, C and Chang, Y 2014, 'Physical Insight into Fuel Mixing Enhancement with BackwardFacing Step for Scramjet Engines via MultiObjective Design Optimization', in Proceedings of ICAS 2014, St. Petersburg, Russia, 712 September 2014, pp. 111.

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Bell, G, Ogawa, H and Watkins, S 2014, 'Numerical investigation on flow control effects of plasma actuators for subsonic aerofoils in turbine applications', in Harun Chowdhury, Firoz Alam (ed.) Proceedings of the 19th Australasian Fluid Mechanics Conference 2014, Melbourne, Australia, 811 December 2014, pp. 14.

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Michael, C, Ogawa, H and Dorrington, G 2014, 'Thrust augmentation by afterburning in a scramjet nozzle', in Harun Chowdhury, Firoz Alam (ed.) Proceedings of the 19th Australasian Fluid Mechanics Conference 2014, Melbourne, Australia, 811 December 2014, pp. 14.

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Ogawa, H, Molder, S, Timofeev, E and Boyce, R 2013, 'Startability and Mach reflection hysteresis of shortened Busemann intakes for axisymmetric scramjet engines', in 29th International Symposium on Shock Waves Volume 1, Madison, United States, 1419 July 2013, pp. 641646.

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Ogawa, H, Molder, S and Boyce, R 2012, 'Numerical investigation of diaphragm mass and viscous effects on pulse starting of axisymmetric scramjet inlets', in P. A. Brandner & B. W. Pearce (ed.) Proceedings of the 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 37 December 2012.

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Ogawa, H, Boyce, R and Molder, S 2012, 'Effects of leadingedge truncation and stunting on drag and efficiency of busemann intakes for axisymmetric scramjet engines', in Shigenao Maruyama (ed.) Proceedings of the Ninth International Conference on Flow Dynamics ICFD2012, Sendai, Japan, 1921 September 2012, pp. 308309.

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Saha, A, Tapabrata, R, Ogawa, H and Boyce, R 2011, 'Learning from evolutionary algorithm based design optimization of axisymmetric scramjet inlets', in Wayne Short, Iver Cairns (ed.) Proceedings of the 11th Australian Space Science Conference Australian Space Science Conference (ASSC 2011), Canberra, Australia, 2629 September 2011, pp. 351357.

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Ogawa, H and Boyce, R 2010, 'Physical insight into nozzle flow behaviour of axisymmetric scramjets for accesstospace via design optimisation', in Wayne Short and Iver Cairns (ed.) Proceedings of the 10th Australian Space Science Conference, Brisbane, Australia, 2730 September 2010, pp. 3950.

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Ogawa, H, Alazet, Y, Boyce, R, Amitay, I and Tapabrata, R 2010, 'Design optimisation of axisymmetric scramjets for accesstospace', in Wayne Short and Iver Cairns (ed.) Proceedings of the 9th Australian Space Science Conference, Sydney, Australia, 28 August  1 October 2009, pp. 143152.

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