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Research Output 2005 2019

2019
2 Citations (Scopus)

Characterization of a 3DOF aeroelastic system with freeplay and aerodynamic nonlinearities – Part I: Higher-order spectra

Candon, M., Carrese, R., Ogawa, H., Marzocca, P., Mouser, C., Levinski, O. & Silva, W. A., Mar 1 2019, In : Mechanical Systems and Signal Processing. 118, p. 781-807 27 p.

Research output: Contribution to journalArticle

Control nonlinearities
Control surfaces
Aerodynamics
Aeroelasticity
Transonic flow
2 Citations (Scopus)

Characterization of a 3DOF aeroelastic system with freeplay and aerodynamic nonlinearities – Part II: Hilbert–Huang transform

Candon, M., Carrese, R., Ogawa, H., Marzocca, P., Mouser, C. & Levinski, O., Jan 1 2019, In : Mechanical Systems and Signal Processing. 114, p. 628-643 16 p.

Research output: Contribution to journalArticle

Aerodynamics
Transonic flow
Control surfaces
Airfoils
Mathematical transformations

Investigation of influence of magnet thickness on performance of cusped field thruster via multi-objective design optimization

Yeo, S. H. & Ogawa, H., Jan 1 2019, The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018. Zhang, X. (ed.). Springer Verlag, p. 1969-1989 21 p. (Lecture Notes in Electrical Engineering; vol. 459).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Magnets
Electric propulsion
Magnetic mirrors
Satellites
Design optimization
1 Citation (Scopus)

Investigation on the performance and feasibility of RBCC-based access-to-space via multi-objective design optimization

Klink, P. & Ogawa, H., Apr 1 2019, In : Acta Astronautica. 157, p. 435-454 20 p.

Research output: Contribution to journalArticle

Rockets
Propulsion
Orbits
Engines
Design optimization

Mixing characteristics of cracked gaseous hydrocarbon fuels in a scramjet combustor

Ravindran, M., Bricalli, M., Pudsey, A. & Ogawa, H., Sep 1 2019, In : Acta Astronautica. 162, p. 168-184 17 p.

Research output: Contribution to journalArticle

Combustors
Hydrocarbons
Residual fuels
Heat sinks
Flow structure

Multi-objective optimization and particle-in-cell simulation of cusped field thruster for micro-satellites platform

Yeo, S. H., Fahey, T., Ogawa, H., Muffatti, A., Matthias, P., Kahnfeld, D., Padivattathumana, M. & Schneider, R., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Multiobjective optimization
Propulsion
Electric propulsion
Satellites
Anodes

Numerical Analysis of Transonic Buffet Control Using a Two-Dimensional Bump for a Supercritical Aerofoil

Yang, Z. & Ogawa, H., Jan 1 2019, The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018. Zhang, X. (ed.). Springer Verlag, p. 854-869 16 p. (Lecture Notes in Electrical Engineering; vol. 459).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Shock waves
Numerical analysis
Boundary layers
Transonic flow

Numerical study of viscous effects on centreline shock reflection in axisymmetric flow

Shoev, G. & Ogawa, H., Feb 1 2019, In : Physics of Fluids. 31, 2, 026105.

Research output: Contribution to journalArticle

axisymmetric flow
shock
configurations
Rankine-Hugoniot relation
implosions

Particle-in-cell simulation of an optimized high-efficiency multistage plasma thruster

Matthias, P., Kahnfeld, D., Schneider, R., Yeo, S. H. & Ogawa, H., Oct 1 2019, In : Contributions to Plasma Physics. 59, 9, e201900028.

Research output: Contribution to journalArticle

design optimization
cells
simulation
chemical propulsion
electric propulsion
2 Citations (Scopus)

Space traffic management: towards safe and unsegregated space transport operations

Hilton, S., Sabatini, R., Gardi, A., Ogawa, H. & Teofilatto, P., Feb 2019, In : Progress in Aerospace Sciences. 105, p. 98-125 28 p.

Research output: Contribution to journalReview article

Navigation
Air
Communication
Orbits
Space debris
2018

Characterization of control surface freeplay with nonstationary aerodynamic loading via the hilbert-huang transform

Candon, M., Carresey, R., Joseph, N., Ogawa, H. & Marzocca, P., Jan 1 2018, AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials. 210049 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018; no. 210049).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Control surfaces
Aerodynamics
Transonic flow
Airfoils
Mathematical transformations
1 Citation (Scopus)

Mixing characteristics of cracked gaseous hydrocarbon fuels in scramjets

Ravindran, M. R., Bricalli, M. G., Pudsey, A. S. & Ogawa, H., Jan 1 2018, 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-5260. (22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

gaseous fuels
hydrocarbon fuels
supersonic combustion ramjet engines
Hydrocarbons
hydrocarbon

Multi-objective design optimization of flow control behind backward facing steps with dielectric barrier discharge plasma actuators

Boom, Y. J., Lio, K. F. & Ogawa, H., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flow control
Actuators
Plasmas
Inlet flow
Flow separation
4 Citations (Scopus)

Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines

Candon, M. J. & Ogawa, H., Jun 1 2018, In : Acta Astronautica. 147, p. 281-296 16 p.

Research output: Contribution to journalArticle

Struts
Numerical analysis
Nozzles
Engines
Hydrogen

Optimization of Backward-Facing Step Flow Control Using Dielectric Barrier Discharge Plasma Actuators

Boom, Y. J., Lio, K. F. & Ogawa, H., Sep 1 2018, In : International Journal of Aeronautical and Space Sciences. 19, 3, p. 595-605 11 p.

Research output: Contribution to journalArticle

Flow control
Actuators
Plasmas
Evolutionary algorithms
Inlet flow
2017

Enceladus plume and icy body exospheric particle sampling using rotating tether and alternative architectures

Dorrington, G. E., Ogawa, H. & Trivailo, P. M., Jan 1 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 3058-3072 15 p. (Proceedings of the International Astronautical Congress, IAC; vol. 5).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Enceladus
plumes
plume
sampling
Sampling
3 Citations (Scopus)

Evolutionary optimization of transonic airfoils for static and dynamic trim performance

Candon, M., Carrese, R., Joseph, N., Ogawa, H. & Marzocca, P., May 1 2017, In : Journal of Intelligent Material Systems and Structures. 28, 8, p. 1071-1088 18 p.

Research output: Contribution to journalArticle

Airfoils
Aerodynamics
Flight envelopes
Evolutionary algorithms
Particle swarm optimization (PSO)

High fidelity multi-objective design optimization of a downscaled cusped field thruster

Fahey, T., Muffatti, A. & Ogawa, H., Jan 1 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 1141-1152 12 p. (Proceedings of the International Astronautical Congress, IAC; vol. 2).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

design optimization
impulses
optimization
Magnets
Anodes
3 Citations (Scopus)

High fidelity multi-objective design optimization of a downscaled Cusped Field Thruster

Fahey, T., Muffatti, A. & Ogawa, H., Dec 1 2017, In : Aerospace. 4, 4, 55.

Research output: Contribution to journalArticle

Open Access
Anodes
Magnets
Flow rate
Hall effect
Beam plasma interactions
1 Citation (Scopus)

Identification and characterization of a nonlinear aeroelastic system with freeplay and aerodynamic nonlinearities via higher–order spectra

Candon, M., Carrese, R., Ogawa, H., Marzocca, P., Mouser, C., Levinskik, O. & Silva, W. A., Jan 1 2017, 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, (58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Control nonlinearities
Nonlinear systems
Identification (control systems)
Aerodynamics
Transonic aerodynamics
1 Citation (Scopus)

Identification of freeplay and aerodynamic nonlinearities in a 2D aerofoil system with via higher-order spectra

Candon, M., Carrese, R., Ogawa, H. & Marzocca, P., Oct 1 2017, In : Aeronautical Journal. 121, 1244, p. 1-29 29 p.

Research output: Contribution to journalArticle

Airfoils
Aerodynamics
Fluid structure interaction
Spectral density
Mach number
3 Citations (Scopus)

Multi-objective design optimization of precoolers for hypersonic airbreathing propulsion

Yu, S., Jones, T., Ogawa, H. & Karwa, N., Jan 1 2017, In : Journal of Thermophysics and Heat Transfer. 31, 2, p. 421-433 13 p.

Research output: Contribution to journalArticle

hypersonics
design optimization
propulsion
tubes
precooling
2016
16 Citations (Scopus)
Fuel injection
Geometry
Orifices
Vorticity
Mach number
3 Citations (Scopus)

Identification of nonlinear aeroelastic behavior of a wing with pitching and plunging freeplay via higher-order spectra analysis

Candon, M., Ogawa, H., Carrese, R. & Marzocca, P., Jan 1 2016, 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Transient analysis
Spectrum analysis
Fluid structure interaction
Structural health monitoring
2015
1 Citation (Scopus)

An investigation into the effect of freeplay on the nonlinear aeroelastic behavior of a wing via higher-order spectra

Candon, M., Ogawa, H., Carrese, R. & Marzocca, P., Jan 1 2015, 26th International Conference on Adaptive Structures and Technologies, ICAST 2015. International Conference on Adaptive Structures and Technologies, (26th International Conference on Adaptive Structures and Technologies, ICAST 2015).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flutter (aerodynamics)
Fluid structure interaction
Modal analysis
Torsional stress
Spectrum analysis

Evolutionary shape optimization of transonic airfoils for aerodynamic and aeroelastic performance

Carrese, R., Marzocca, P., Candon, M. & Ogawa, H., Jan 1 2015, 26th International Conference on Adaptive Structures and Technologies, ICAST 2015. International Conference on Adaptive Structures and Technologies, (26th International Conference on Adaptive Structures and Technologies, ICAST 2015).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shape optimization
Airfoils
Aerodynamics
Flight envelopes
Multiobjective optimization
1 Citation (Scopus)

Flow analysis of the effect of tube geometry on the performance of pre-coolers for turbine-based hypersonic air-breathing propulsion

Jones, T., Karwa, N., Ogawa, H. & Rosengarten, G., Jan 1 2015, p. 500-509. 10 p.

Research output: Contribution to conferencePaper

Hypersonic aerodynamics
Propulsion
Turbines
Hypersonic vehicles
Geometry
1 Citation (Scopus)

Investigation on Effective Sampling Strategy for Multi-objective Design Optimization of RBCC Propulsion Systems via Surrogate-assisted Evolutionary Algorithms

Ho, T. Q., Ogawa, H. & Bil, C., Jan 1 2015, In : Procedia Engineering. 99, p. 1252-1262 11 p.

Research output: Contribution to journalConference article

Open Access
Rockets
Evolutionary algorithms
Propulsion
Sampling
Engines
8 Citations (Scopus)
fuel injection
supersonic combustion ramjet engines
Fuel injection
injectors
upstream
1 Citation (Scopus)

Numerical investigation of upstream fuel injection through porous media for scramjet engines via surrogate-assisted evolutionary algorithms

Ogawa, H., Capra, B. & Lorrain, P., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0884. (53rd AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fuel injection
Evolutionary algorithms
Porous materials
Engines
Sensitivity analysis

Numerical investigation on the efficiency of a plasma actuator for turbine applications

Bell, G., Ogawa, H. & Watkins, S., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0306. (53rd AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Turbines
Actuators
Plasmas
Electric power utilization
Aerodynamic drag

Physical insight into fuel/air mixing with hypermixer injectors for scramjet engines

Ogawa, H. & Kodera, M., Jan 1 2015, In : Journal of Guidance, Control, and Dynamics. 38, 6, p. 1423-1435 13 p.

Research output: Contribution to journalArticle

Scramjet
supersonic combustion ramjet engines
Injector
injectors
engine
8 Citations (Scopus)
supersonic combustion ramjet engines
design optimization
fuel injection
upstream
Fuel injection

Thrust augmentation optimization through supersonic after-burning in scramjet engine nozzles via surrogate-assisted evolutionary algorithms

Candon, M. J., Ogawa, H. & Dorrington, G. E., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-1106. (53rd AIAA Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Evolutionary algorithms
Nozzles
Engines
Nozzle design
Hypersonic aerodynamics
4 Citations (Scopus)

Thrust augmentation through after-burning in scramjet nozzles

Candon, M. J., Ogawa, H. & Dorrington, G. E., Apr 1 2015, In : Advances in Aircraft and Spacecraft Science. 2, 2, p. 183-198 16 p.

Research output: Contribution to journalArticle

Nozzles
Nozzle design
Hypersonic aerodynamics
Stress concentration
Shear stress
2014
6 Citations (Scopus)

Multi-objective design and trajectory optimization of space transport systems with RBCC propulsion via evolutionary algorithms and pseudospectral methods

Kodera, M., Ogawa, H., Tomioka, S. & Ueda, S., Jan 1 2014, 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., (52nd Aerospace Sciences Meeting).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Rockets
Evolutionary algorithms
Propulsion
Trajectories
Mach number
7 Citations (Scopus)

Multi-phase trajectory optimization for access-to-space with RBCC-powered TSTO via surrogated-assisted hybrid evolutionary algorithms incorporating pseudo-spectral methods

Ogawa, H., Kodera, M., Tomioka, S. & Ueda, S., Jan 1 2014, AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. American Institute of Aeronautics and Astronautics Inc., (AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Rockets
Evolutionary algorithms
Orbits
Trajectories
Rocket engines
1 Citation (Scopus)

Numerical investigation on flow control effects of plasma actuators for subsonic aerofoils in turbine applications

Bell, G. W., Ogawa, H. & Watkins, S., Jan 1 2014, Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014. Australasian Fluid Mechanics Society, (Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Flow control
Turbines
Actuators
Plasmas

Physical insight into fuel mixing enhancement with backward-facing step for scramjet engines via multi-objective design optimization

Ogawa, H., Wen, C. Y. & Chang, Y. C., Jan 1 2014, 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014. International Council of the Aeronautical Sciences, (29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Engines
Fuel injection
Evolutionary algorithms
Propulsion
Sensitivity analysis

Simulation and experimental testing of Leonardo da Vinci's helical rotor

Dorrington, G. E., Ogawa, H., McCarthy, J. & Carrese, R., Jan 1 2014, Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014. Australasian Fluid Mechanics Society, (Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Rotors
Free flight
Flow simulation
Testing

Thrust augmentation by after-burning in a scramjet nozzle

Candon, M. J., Ogawa, H. & Dorrington, G. E., Jan 1 2014, Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014. Australasian Fluid Mechanics Society, (Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Nozzles
Stress concentration
Shear stress
Oxygen
Liquids
2013
3 Citations (Scopus)

Computational investigation of fuel injection with various injector geometries and mixing into hypersonic crossflow in scramjet engines

Ogawa, H. & Boyce, R. R., Aug 19 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013. (51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

fuel injection
supersonic combustion ramjet engines
hypersonics
Hypersonic aerodynamics
Fuel injection
2012
13 Citations (Scopus)

Multi-objective design optimization of fuel injection for mixing enhancement in scramjets by using surrogate-assisted evolutionary algorithms

Ogawa, H. & Boyce, R. R., Dec 1 2012, 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. (18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

fuel injection
supersonic combustion ramjet engines
Fuel injection
design optimization
injectors
22 Citations (Scopus)

Nozzle design optimization for axisymmetric scramjets by using surrogate-assisted evolutionary algorithms

Ogawa, H. & Boyce, R. R., Nov 1 2012, In : Journal of Propulsion and Power. 28, 6, p. 1324-1338 15 p.

Research output: Contribution to journalArticle

nozzle design
Nozzle design
supersonic combustion ramjet engines
design optimization
Evolutionary algorithms

Numerical investigation of diaphragm mass and viscous effects on pulse starting of axisymmetric scramjet inlets

Ogawa, H., Mölder, S. & Boyce, R. R., Jan 1 2012, Proceedings of the 18th Australasian Fluid Mechanics Conference, AFMC 2012. Brandner, P. A. & Pearce, B. W. (eds.). Australasian Fluid Mechanics Society, (Proceedings of the 18th Australasian Fluid Mechanics Conference, AFMC 2012).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Diaphragms
Inlet flow
Hypersonic aerodynamics
Unsteady flow
Viscosity
22 Citations (Scopus)

Physical insight into scramjet inlet behavior via multi-objective design optimization

Ogawa, H. & Boyce, R. R., Aug 1 2012, In : AIAA journal. 50, 8, p. 1773-1783 11 p.

Research output: Contribution to journalArticle

Drag
Geometry
Pressure gradient
Evolutionary algorithms
Propulsion

Robust design optimization of high-performance axisymmetric scramjets based on surrogate-assisted evolutionary algorithms

Saha, A., Ray, T., Ogawa, H. & Boyce, R., Dec 1 2012, 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012. p. 2534-2544 11 p. (28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012; vol. 3).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Evolutionary algorithms
Hypersonic aerodynamics
Aerodynamic loads
Aerospace applications
Rocket engines
4 Citations (Scopus)

The unsteady flow physics of hypersonic inlet starting processes

Grainger, A. L., Boyce, R. R., Tirtey, S. C., Ogawa, H., Paniagua, G. & Paris, S., Dec 1 2012, 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. (18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

hypersonic inlets
Hypersonic inlets
unsteady flow
Unsteady flow
flow field
2011
4 Citations (Scopus)

Full flow-path optimization of axisymmetric scramjet engines

Ogawa, H., Alazet, Y., Pudsey, A., Boyce, R. R., Isaacs, A. & Ray, T., Dec 1 2011, 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011. (17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

supersonic combustion ramjet engines
Fuel injection
fuel injection
engine
Engines