Article contents
An Empirical Formula for Stagnation Point Velocity Gradient for Spheres and Circular Cylinders in Hypersonic Flow
Published online by Cambridge University Press: 04 July 2016
Extract
When stagnation heat transfer rates are expressed in terms of free stream flow properties, the following combination of terms is found to occur: —
where ps pressure at the stagnation point
p∞free stream pressure
U∞free stream velocity
Dnose diameter
ßstagnation point velocity gradient.
- Type
- Technical Notes
- Information
- Copyright
- Copyright © Royal Aeronautical Society 1965
References
- 1
- Cited by