Detached Shock Waves around Cylinders Flying at Mach Number Ranging from 1 to 2

• MIZUKAKI T.

  The First Research Center, Technical Research and Development Institute, Japan Defense Agency

Journal

• Journal of visualization

  Journal of visualization 11 (2), 133-141, 2008-04-01

Keywords

• Flow visualization
• High-speed projectiles
• Detached shock waves

Details

• CRID: 1574231875325401216
• NII Article ID: 10021111294
• NII Book ID: AA11268703
• ISSN: 13438875
• Text Lang: en
• Data Source:
  • CiNii Articles