Abstract
Five-mm-diameter projectiles, whose speed was beyond the Chapman-Jouguet (C-J) detonation speed, were fired into mixtures containing stoichiometric hydrogen-oxygen gases plus argon diluents. The flowfield around the projectile was visualized using a CCD camera. We measured the minimum normal velocity components of detonation waves around the projectiles and the effective curvature radius of a bow detonation wave near the projectile tip. From these experimental results we concluded that the steady-state C-J detonation wave is stabilized around a projectile when the effective curvature radius of the bow detonation wave is larger than 8.6 times of the detonation cell size.
Original language | English |
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Publication status | Published - 2001 Dec 1 |
Event | 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001 - Kyoto, Japan Duration: 2001 Apr 24 → 2001 Apr 27 |
Other
Other | 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001 |
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Country/Territory | Japan |
City | Kyoto |
Period | 01/4/24 → 01/4/27 |
ASJC Scopus subject areas
- Space and Planetary Science
- Aerospace Engineering
- Control and Systems Engineering