• 524 Citations
  • 11 h-Index
20022020

Research output per year

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Article
2020

Multiobjective optimization and particle-in-cell simulation of cusped field thrusters for microsatellite platforms

Yeo, S. H., Ogawa, H., Matthias, P., Kahnfeld, D. & Schneider, R., 2020, In : Journal of Spacecraft and Rockets. 57, 3, p. 603-611 9 p.

Research output: Contribution to journalArticle

Numerical investigation of upstream cavity enhanced fuel mixing in scramjet combustors

Roos, T., Pudsey, A., Bricalli, M. & Ogawa, H., Apr 2020, In : Acta Astronautica. 169, p. 50-65 16 p.

Research output: Contribution to journalArticle

2019

Cavity enhanced jet interactions in a scramjet combustor

Roos, T., Pudsey, A., Bricalli, M. & Ogawa, H., Apr 2019, In : Acta Astronautica. 157, p. 162-179 18 p.

Research output: Contribution to journalArticle

4 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

4 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

4 Citations (Scopus)

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

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

Research output: Contribution to journalArticle

2 Citations (Scopus)

Mixing characteristics of cracked gaseous hydrocarbon fuels in a scramjet combustor

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

Research output: Contribution to journalArticle

3 Citations (Scopus)

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

1 Citation (Scopus)

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

1 Citation (Scopus)
2018

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

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

Research output: Contribution to journalArticle

6 Citations (Scopus)

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

2017

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

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
4 Citations (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

1 Citation (Scopus)

Multi-objective design optimization of precoolers for hypersonic airbreathing propulsion

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

Research output: Contribution to journalArticle

7 Citations (Scopus)
2016
23 Citations (Scopus)
2015
8 Citations (Scopus)

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

Ogawa, H. & Kodera, M., 2015, In : Journal of Propulsion and Power. 38, 6, p. 1423-1435 13 p.

Research output: Contribution to journalArticle

10 Citations (Scopus)
9 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

6 Citations (Scopus)
2013
2012

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

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

Research output: Contribution to journalArticle

23 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

23 Citations (Scopus)
2010

Inlet starting of high-contraction axisymmetric scramjets

Ogawa, H., Grainger, A. L. & Boyce, R. R., 2010, In : Journal of Propulsion and Power. 26, 6, p. 1247-1258 12 p.

Research output: Contribution to journalArticle

38 Citations (Scopus)

Multi-Objective Design Optimisation of Inlet and Combustor for Axisymmetric Scramjets

Ogawa, H., Boyce, R., Isaacs, A. & Ray, T., 2010, In : Open Thermodynamics Journal. 4, 6, p. 86-91

Research output: Contribution to journalArticle

2008

SBLI control for wings and inlets

Babinsky, H. & Ogawa, H., Jul 2008, In : Shock Waves. 18, 2, p. 89-96 8 p.

Research output: Contribution to journalArticle

56 Citations (Scopus)

Shock-wave/boundary-layer interaction control using three-dimensional bumps for transonic wings

Ogawa, H., Babinsky, H., M. Pätzold, P. & T. Lutz, L., Jun 1 2008, In : AIAA journal. 46, 6, p. 1442-1452 11 p.

Research output: Contribution to journalArticle

93 Citations (Scopus)
2006

Evaluation of wave drag reduction by flow control

Ogawa, H. & Babinsky, H., Jan 1 2006, In : Aerospace Science and Technology. 10, 1, p. 1-8 8 p.

Research output: Contribution to journalArticle

22 Citations (Scopus)

Wind-tunnel setup for investigations of normal shock wave/boundary-layer interaction control

Ogawa, H. & Babinsky, H., Nov 1 2006, In : AIAA journal. 44, 11, p. 2803-2805 3 p.

Research output: Contribution to journalArticle

42 Citations (Scopus)
2002

Fore-Body Drag Reduction of a Blunt Body in Compressible Turbulent Boundary Layer

Yamawaki, T., Ogawa, H., Okunuki, T., Koyama, H., Itoh, H. & Morishita, E., 2002, In : Transactions of the Japan Society for Aeronautical and Space Sciences. 50, 586, p. 474-476

Research output: Contribution to journalArticle