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

Satoshi Sumiya, Shinichi Maeda, Jiro Kasahara, Akiko Matsuo

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

Abstract

A detonable mixture was ignited by hypersonic spherical projectiles whose velocities we Self-propagated detonation wave has important relationship for reflection by wall surface which causes the fatal difference of pressure and temperature. In this study, we figured out experimentally the influence by curvature of oblique detonation waves (ODWs) around hypersonic spherical projectiles. And we compared to require the boundary condition on flow region by the measurement of incident detonataion wave angle for two reflection model of normal reflection and mach reflection. A detonable mixture (2C<inf>2</inf>H<inf>2</inf>+5O<inf>2</inf>+7Ar) was ignited by hypersonic spherical projectiles whose velocities were about 1.2 times of Chapman-Jouget (C-J) velocity. Using Schlieren imaging system and high speed video camera, we directly visualized detailed time history (1 μs intervals) about the reflection model of ODW.So , we revealed the curvature influence for the reflection.

Original languageEnglish
Title of host publication52nd Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624102561
Publication statusPublished - 2014
Event52nd Aerospace Sciences Meeting 2014 - National Harbor, United States
Duration: 2014 Jan 132014 Jan 17

Other

Other52nd Aerospace Sciences Meeting 2014
CountryUnited States
CityNational Harbor
Period14/1/1314/1/17

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ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Sumiya, S., Maeda, S., Kasahara, J., & Matsuo, A. (2014). Reflection Phenomena of oblique detonation wave around hypersonic spherical projectiles on plane plate. In 52nd Aerospace Sciences Meeting American Institute of Aeronautics and Astronautics Inc..