Hypersonic flow
- Title
- Hypersonic flow
- Collection
- Caltech Images Collection
- Series
- Academic Divisions and Departments
- Sub-Series
- Aerospace (Aeronautics)
- Identifier
- 10.9-21
- Extents
- 1 photographs (negative)
- Abstract
- Helium ejected from nose cone in wind tunnel at 5.8 Mach pushes shock wave away from nose cone in cooling effect.