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Research Output 1993 2019

  • 1335 Citations
  • 20 h-Index
  • 96 Article
  • 86 Conference contribution
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Conference contribution
2019
1 Citation (Scopus)

Experimental performance validation of a rotating detonation engine toward a flight demonstration

Goto, K., Yokoo, R., Kim, J., Kawasaki, A., Matsuoka, K., Kasahara, J., Matsuo, A., Funaki, I., Nakata, D. & Uchiumi, M., 2019 Jan 1, 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

Detonation
Demonstrations
Engines
Oxygen
Methane
1 Citation (Scopus)

Propulsion performance of inner-cylinder-less rotating detonation engine

Yokoo, R., Goto, K., Kim, J., Kawasaki, A., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2019 Jan 1, 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

Detonation
Engine cylinders
Combustion chambers
Propulsion
Engines

Research and development of rotating detonation engine system for the sounding rocket flight experiment S520-31

Kasahara, J., Kawasaki, A., Matsuoka, K., Matsuo, A., Funaki, I., Nakata, D. & Uchiumi, M., 2019 Jul 18, 8th BSME International Conference on Thermal Engineering. Sadrul Islam, A. K. M., Ruhul Amin, M. & Ali, M. (eds.). American Institute of Physics Inc., 020001. (AIP Conference Proceedings; vol. 2121).

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

Open Access
rocket flight
sounding rockets
engines
research and development
detonation

The effect of acceleration and exit velocity on hypersonic projectiles launched by a ground-based railgun

Kasahara, H. & Matsuo, A., 2019 Jan 1, 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

Rail guns
Hypersonic aerodynamics
Projectiles
Shock waves
Mach number
2018
2 Citations (Scopus)

Numerical investigation of the gas-particle flow in the shock tube using discrete particle and continuum model

Kimura, A. & Matsuo, A., 2018 Jan 1, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3550

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

Shock tubes
Shock waves
Gases
Computational fluid dynamics
Fluids
4 Citations (Scopus)

Preliminary experiments on rotating detonation rocket engine for flight demonstration using sounding rocket

Goto, K., Nishimura, J., Higashi, J., Taki, H., Ukai, T., Hayamizu, Y., Kikuchi, K., Yamada, T., Watanabe, S., Hotta, K., Inakawa, T., Kubota, A., Yamaguchi, M., Daicho, T., Kawasaki, A., Matsuoka, K., Kasahara, J., Matsuo, A., Funaki, I., Yasuda, K. & 5 others, Mori, K., Yagihashi, H., Nakata, D., Uchiumi, M. & Higashino, K., 2018 Jan 1, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Sounding rockets
Rocket engines
Detonation
Demonstrations
Engines

The effect of exit velocity and material on the sabot separation launched by ground-based railgun

Kasahara, H. & Matsuo, A., 2018 Jan 1, 2018 Applied Aerodynamics Conference. [publishername] American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3819

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

Rail guns
Computational fluid dynamics
Trajectories
Hypersonic aerodynamics

The effect of shape on the aerodynamic and thermal performance of hypersonic projectiles launched by a ground-based railgun

Kasahara, H. & Matsuo, A., 2018 Jan 1, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Rail guns
Hypersonic aerodynamics
Projectiles
Aerodynamics
Free flight
2017
14 Citations (Scopus)

Experimental study of disk-shaped rotating detonation Turbine engine

Higashi, J., Ishiyama, C., Nakagami, S., Matsuoka, K., Kasahara, J., Matsuo, A., Funaki, I. & Moriai, H., 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-1286

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

Detonation
Turbines
Radial flow
Centrifugal compressors
Experiments
3 Citations (Scopus)

Numerical investigation on burned gas backflow in liquid fuel purge method

Watanabe, H., Matsuo, A., Matsuoka, K. & Kasahara, J., 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-1284

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

Liquid fuels
Ignition
Propellants
Gases
Purging
7 Citations (Scopus)

Study on a long-time operation towards rotating detonation rocket engine flight demonstration

Ishihara, K., Nishimura, J., Goto, K., Nakagami, S., Matsuoka, K., Kasahara, J., Matsuo, A., Funaki, I., Moriai, H., Mukae, H., Yasuda, K., Nakata, D. & Higashino, K., 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-1062

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

Rocket engines
Detonation
Demonstrations
Engines
Sea level
2016

Development of high-frequency pulse detonation combustor without purging material

Muto, K., Matsuoka, K., Kasahara, J., Watanabe, H., Matsuo, A. & Endo, T., 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Purging
Detonation
Combustors
Oxygen
Ethylene
1 Citation (Scopus)

Experimental performance evaluation of 3N-class pulse detonation thruster using liquid purge method

Takagi, S., Hosono, K., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Detonation
Liquids
Combustors
Monopropellants
Engines
5 Citations (Scopus)

Experimental study of effects of injector configurations on rotating detonation engine performance

Goto, K., Kato, Y., Ishihara, K., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2016, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Detonation
Engines
Propellants
Combustion chambers
Gas turbines
9 Citations (Scopus)

Experimental study of research of centrifugal-compressor-radial-turbine type rotating detonation engine

Ishiyama, C., Miyazaki, K., Nakagami, S., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2016, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Centrifugal compressors
Detonation
Turbines
Engines
Aircraft

Numerical simulation towards investigating the factor for velocity decrease of detonation wave in rotating detonation engine chamber

Fujii, J., Kumazawa, Y., Matsuo, A., Nakagami, S., Matsuoka, K. & Kasahara, J., 2016, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Detonation
Engines
Computer simulation
Gases
Nozzles
1 Citation (Scopus)

Numerical study for rotating detonation propagation in a two-parallel-plane combustor

Kumazawa, Y., Fujii, J., Matsuo, A., Nakagami, S., Matsuoka, K. & Kasahara, J., 2016, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Detonation
Combustors
Euler equations
Propellants
Gases
1 Citation (Scopus)

One-Dimensional numerical investigation on purging the burned gas by the evaporation of water droplets in pulse detonation combustor

Watanabe, H., Matsuo, A., Muto, K., Matsuoka, K., Kasahara, J. & Endo, T., 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Purging
Detonation
Combustors
Evaporation
Gases
5 Citations (Scopus)

Study of combustion chamber characteristic length in rotating detonation engine with convergent-divergent nozzle

Kato, Y., Ishihara, K., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-9 9 p.

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

Detonation
Combustion chambers
Combustors
Nozzles
Engines
2015
1 Citation (Scopus)

Numerical investigation of shock-induced combustion with unsteady oscillation around hypervelocity conical projectile

Maeda, K. & Matsuo, A., 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-1824

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

Projectiles
Shock waves
Geometry
Euler equations
9 Citations (Scopus)

Performance evaluation of a rotating detonation engine with conical-shape tail

Ishihara, K., Kato, Y., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0630

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

Detonation
Engines
Rocket engines
Propellants
Gases
2 Citations (Scopus)

Schlieren-system-visualization of combustion phenomena in a two-parallel-plane rotating detonation combustor

Nakagami, S., Matsuoka, K., Kasahara, J., Kumazawa, Y., Matsuo, A. & Funaki, I., 2015, 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

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

Schlieren systems
Detonation
Combustors
Visualization
Combustion chambers
13 Citations (Scopus)

Visualization of rotating detonation waves in a plane combustor with a cylindrical wall injector

Nakagami, S., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0878

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

Detonation
Combustors
Visualization
Engines
Gas turbines
2014
1 Citation (Scopus)

Ejector configuration for designing a simple and high performance solar cooling system

Saito, Y., Ito, T., Matsuo, A. & Sato, H., 2014, Energy Procedia. Elsevier Ltd, Vol. 57. p. 2564-2571 8 p.

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

Cooling systems
Cooling
Refrigerants
Refrigeration
Nozzles

Flight demonstration of a pulse detonation rocket system todoroki II

Matsuoka, K., Takagi, S., Kasahara, J., Morozumi, T., Matsuo, A. & Funaki, I., 2014, Proceedings of the International Astronautical Congress, IAC. International Astronautical Federation, IAF, Vol. 10. p. 7529-7534 6 p.

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

Detonation
Rockets
detonation
rockets
thrust

Reflection phenomena of oblique detonation wave around hypersonic spherical projectiles on plane plate

Sumiya, S., Maeda, S., Kasahara, J. & Matsuo, A., 2014, 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc.

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

detonation waves
hypersonics
Hypersonic aerodynamics
Detonation
Projectiles

Reflection Phenomena of oblique detonation wave around hypersonic spherical projectiles on plane plate

Sumiya, S., Maeda, S., Kasahara, J. & Matsuo, A., 2014, 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc.

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

Hypersonic aerodynamics
Detonation
Projectiles
High speed cameras
Video cameras
7 Citations (Scopus)

Study on a rotary-valved four-cylinder pulse detonation rocket: Six degree-of-freedom flight measurement

Matsuoka, K., Takagi, S., Kasahara, J., Morozumi, T., Kashiwazaki, T., Fujiwara, Y., Matsuo, A. & Funaki, I., 2014, 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc.

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

Detonation
Engine cylinders
Rockets
Propellants
Demonstrations
2 Citations (Scopus)

Study on a rotary-valved four-cylinder pulse detonation rocket: Six degree-of-freedom flight measurement

Matsuoka, K., Takagi, S., Kasahara, J., Morozumi, T., Kashiwazaki, T., Fujiwara, Y., Matsuo, A. & Funaki, I., 2014, 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc.

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

Detonation
Engine cylinders
Rockets
detonation
rockets
7 Citations (Scopus)

Study on a rotary-valved four-cylinder pulse detonation rocket: Thrust measurement by ground test

Morozumi, T., Sakamoto, R., Kashiwazaki, T., Matsuoka, K., Takagi, S., Kasahara, J., Matsuo, A. & Funaki, I., 2014, 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc.

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

Detonation
Rockets
Pulse detonation engines
Rocket engines
Gases
2 Citations (Scopus)

Study on Pulse Detonation Rocket Engine using flight test demonstrator “Todoroki II”

Takagi, S., Morozumi, T., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc.

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

Pulse detonation engines
Rocket engines
Propellants
Detonation
Engine cylinders
5 Citations (Scopus)

Thrust measurement of rotating detonation engine by sled test

Kato, Y., Ishihara, K., Gawahara, K., Matsuoka, K., Kasahara, J., Matsuo, A. & Funaki, I., 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc.

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

Detonation
Engines
Rocket engines
Degrees of freedom (mechanics)
Propellants
2013
7 Citations (Scopus)

Detonation engine development for reaction control systems of a spacecraft

Gawahara, K., Nakayama, H., Kasahara, J., Matsuoka, K., Tomioka, S., Hiraiwa, T., Matsuo, A. & Funaki, I., 2013, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.

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

Detonation
Spacecraft
Engines
Control systems
Pressure sensors
1 Citation (Scopus)

Detonation engine development for reaction control systems of a spacecraft

Gawahara, K., Nakayama, H., Kasahara, J., Matsuoka, K., Tomioka, S., Hiraiwa, T., Matsuo, A. & Funaki, I., 2013 Jan 1, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc., (49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference; vol. 1 PartF).

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

Detonation
Spacecraft
Engines
Control systems
Pressure sensors
3 Citations (Scopus)

Numerical investigation of sabot separation process in a ballistic range using moving overlapped grid method

Takeuchi, F. & Matsuo, A., 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013.

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

ballistic ranges
Ballistics
Projectiles
grids
projectiles
3 Citations (Scopus)

Study on a four-cylinder pulse detonation rocket engine with a coaxial high frequency rotary valve

Morozumi, T., Matsuoka, K., Sakamoto, R., Fujiwara, Y., Kasahara, J., Matsuo, A. & Funaki, I., 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013.

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

Pulse detonation engines
rocket engines
pulse detonation engines
Rocket engines
Engine cylinders
2 Citations (Scopus)

Study on detonation wave attenuation through narrow tube for application to explosion safety and detonation engines

Uruno, T., Maeda, S., Kasahara, J. & Matsuo, A., 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013.

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

wave attenuation
detonation waves
Detonation
detonation
Explosions
2 Citations (Scopus)

Three dimensional numerical investigation of the clustered linear aerospike nozzle's flow affected by changing the distance between neighboring cell nozzles

Miyazawa, T., Matsuo, A., Takahashi, H., Tomita, T. & Tomioka, S., 2013, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.

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

Nozzles
Pressure distribution
Airframes
Shock waves
Mach number

Three dimensional numerical investigation of the clustered linear aerospike nozzle’s flow affected by changing the distance between neighboring cell nozzles

Miyazawa, T., Matsuo, A., Takahashi, H., Tomita, T. & Tomioka, S., 2013 Jan 1, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc., (49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference; vol. 1 PartF).

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

Nozzles
Pressure distribution
Airframes
Shock waves
Mach number
2012

An ejector refrigeration cycle for utilizing solar thermal energy

Saito, Y., Fukushima, T., Ito, T., Chan, S., Matsuo, A. & Sato, H., 2012, World Renewable Energy Forum, WREF 2012, Including World Renewable Energy Congress XII and Colorado Renewable Energy Society (CRES) Annual Conferen. Vol. 1. p. 82-87 6 p.

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

Refrigeration
Thermal energy
Cooling
Solar energy
Temperature
1 Citation (Scopus)

Calculation of drag coefficients for hypersonic spherical projectiles initiating oblique detonation wave or shock-induced combustion

Choi, J. Y., Maeda, S., Kasahara, J. & Matsuo, A., 2012, 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2012-0983

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

Drag coefficient
Hypersonic aerodynamics
Detonation
Projectiles
Computational fluid dynamics
1 Citation (Scopus)

Front shock behavior of stable detonation waves propagating through rectangular cross-section curved channels

Nakayama, H., Moriya, T., Kasahara, J., Matsuo, A. & Funaki, I., 2012, 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. AIAA 2012-0618

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

Detonation
Gas mixtures
Visualization
2011

Development of ejector cycle for solar air-conditioning system powered by stored thermal energy Part 1. Experimental results

Fukushima, T., Chan, S., Matsuo, A. & Sato, H., 2011, 30th ISES Biennial Solar World Congress 2011, SWC 2011. Vol. 4. p. 2830-2835 6 p.

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

Thermal energy
Air conditioning
1 Citation (Scopus)

Development of ejector cycle for solar air-conditioning system powered by stored thermal energy part 2. CFD analysis for ejector design

Ito, T., Sato, H. & Matsuo, A., 2011, 30th ISES Biennial Solar World Congress 2011, SWC 2011. Vol. 4. p. 2822-2829 8 p.

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

Thermal energy
Air conditioning
Computational fluid dynamics

On cross-flow mixing parameters in presence of pseudo-shock wave system

Tomioka, S., Sakuranaka, N., Nagatomi, F., Ohkoshi, M., Kobayashi, T. & Matsuo, A., 2011, 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011.

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

Shock waves
Jet fuel
Ducts
Aspect ratio
Flow rate
4 Citations (Scopus)

Thrust measurement and visualization experiment of a multi-cycle single-tube pulse detonation

Matsuoka, K., Esumi, M., Ikeguchi, K. B., Kasahara, J., Matsuo, A. & Funaki, I., 2011, 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011.

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

Pulse detonation engines
Detonation
Rocket engines
Visualization
Ignition
2010

Mixing control by wall flush-mount injectors in dual-mode combustor

Tomioka, S., Izumikawa, M., Sakuranaka, N., Shibata, H., Yamasaki, H., Kobayashi, T. & Matsuo, A., 2010, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2010-6959

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

Combustors
Orifices
Jet fuel
Shock waves
Mach number
2 Citations (Scopus)

Net impulse measurements of pulse detonation tube by using fuel-air mixture

Takeuchi, S., Doi, N., Kasahara, J., Murayama, M. & Matsuo, A., 2010, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-0148

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

Detonation
Air
Pulse detonation engines
Pendulums
Diaphragms

Numerical evaluation of aerodynamic interference between wing and fuselage for hypersonic experimental aircraft

Tanabe, A., Matsuo, A., Kojima, T. & Taguchi, H., 2010, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-1046

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

Fuselages
Hypersonic aerodynamics
Hypersonic vehicles
Aerodynamics
Aircraft
3 Citations (Scopus)

Numerical prediction of interior ballistics performance of projectile accelerator by solid/gas two-phase reacting flow simulation

Miura, H., Matsuo, A. & Nakamura, Y., 2010, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-1145

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

Solid propellants
Flow simulation
Projectiles
Ballistics
Two phase flow