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Preliminary Surface Pressure Measurements of Transitional , Hypersonic Shock Boundary Layer Interactions
| Content Provider | Semantic Scholar |
|---|---|
| Author | Frank, A. J. |
| Copyright Year | 2006 |
| Abstract | A lamlnar boundary layer a t Mach 8 In alr under perfect gas condltlons was subjected t o a shock lnteractlon generated by a sharp ramp of 10 or 20 deg. T h e Reynolds number o f the lnteractlon was 2.27 mllllon. It was found that the lnteractlon stretches over a large extent a n d t h e lnvlscld downstream pressure was not obtalned wlthln the test region. Moreover, I t was found that surface pressure disturbances were damped out rapldly. Based o n the surface pressure measurements, it 1s concluded that the shocks created were not s trong |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://arc.uta.edu/publications/cp_files/AIAA-1996-4541.pdf |
| Language | English |
| Access Restriction | Open |
| Subject Keyword | Degenerative polyarthritis Downstream (software development) RAMP Simulation Software for Modelling Reliability, Availability and Maintainability Shock adenotonsillectomy |
| Content Type | Text |
| Resource Type | Article |
