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| Content Provider | IEEE Xplore Digital Library |
|---|---|
| Author | Pandian, S. Raveendran, P.G. Srinivasan, K. Subramanian, S. Subash, A.N. |
| Copyright Year | 2005 |
| Description | Author affiliation: Vikram Sarabhai Space Centre (VSSC), Indian Space Research Organisation, Thiruvananthapuram-695 022, INDIA. Email: s_pandian@vssc.org (Pandian, S.) |
| Abstract | At hypersonic Mach numbers, the separated boundary layer from the model base develops as a shear layer and separates the outer in-viscid hypersonic flow from low subsonic flow in the base region. Characterizing such a complex mixed hypersonic flow of the base region in a short duration facility needs adequate runtime since base flow itself takes few milliseconds to establish as well as fast response sensors and instrumentation. In the present study fast response sensors are developed and time taken to establish base flow on a typical blunt body is calculated. These experiments were carried out in a shock tunnel at free stream Mach number of 6 and free stream Reynolds number of 0.2 million. To gain additional confidence on the base heat transfer distribution, steady pressure measurements were also carried out in a conventional hypersonic wind tunnel. The studies indicate that for the above test conditions, the heat transfer and pressure distribution on the blunt body base plane is nearly uniform. The time required for the base flow establishment is 1.27 milli seconds. |
| Starting Page | 342 |
| Ending Page | 347 |
| File Size | 4983829 |
| Page Count | 6 |
| File Format | |
| ISBN | 0780390962 |
| DOI | 10.1109/ICIASF.2005.1569942 |
| Language | English |
| Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Publisher Date | 2005-08-29 |
| Publisher Place | Japan |
| Access Restriction | Subscribed |
| Rights Holder | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subject Keyword | Instruments Heat transfer Electric shock Fluid flow measurement Pressure measurement Testing Time measurement Sensor phenomena and characterization Temperature Neck heat transfer rate Base flow Flow establishment time |
| Content Type | Text |
| Resource Type | Article |
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