Hypersonic flow
- Title
- Hypersonic flow
- Collection
- Caltech Images Collection
- Series
- Academic Divisions and Departments
- Sub-Series
- Aerospace (Aeronautics)
- Identifier
- 10.9-18
- Extents
- 1 photographs
- Abstract
- Shock waves about a cone in the hypersonic wind tunnel at a Mach number of 5.8. the crossed waves are not in the airstream.