Mirels, 1964 - Google Patents
Shock tube test time limitation due to turbulentwall boundary layerMirels, 1964
- Document ID
- 11010341053586955098
- Author
- Mirels H
- Publication year
- Publication venue
- AIAA Journal
External Links
Snippet
Shock tube test time limitation due to the premature arrival of the contact surface is analytically investigated for wholly turbulent-wall boundary layers The results are compared with those for wholly laminar-wall boundary layers It is found that, for a given shock Mach …
- 230000035939 shock 0 title abstract description 198
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