| Autor: |
Gai, S. L., Mudford, N. R. |
| Zdroj: |
Shock Waves; March 1992, Vol. 2 Issue: 1 p43-47, 5p |
| Abstrakt: |
The paper describes stagnation point heat flux measurements at a range of enthalpies relevant to re-entry speeds of aero-assisted space transfer vehicles (ASTVs) and proposed space planes, using the Australian National University Free Piston Shock Tunnel T3. The unique feature of these experiments is that they were conducted in the ‘straight through’ (reflectionless) mode which enabled higher enthalpies and densities hitherto unattained. |
| Databáze: |
Supplemental Index |
| Externí odkaz: |
|
Full text from SpringerLink