Abstract
An experimental investigation has been carried out to examine heat-transfer characteristics of an axisymmetric, under-expanded, sonic jet impinging on a flat plate and the local measurement of surface pressures and heat transfer coefficients on a plate have been achieved together with a visualization test of shock structure in a jet. Heat transfer coefficients on a plate have been found to be changed significantly depending on the under-expansion ratio as much as the nozzle-to-plate distance and these phenomena have been explained with other results and discussions by other researchers.
Original language | English |
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Pages | 1165-1172 |
Number of pages | 8 |
DOIs | |
Publication status | Published - 2004 |
Event | 42nd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: 2004 Jan 5 → 2004 Jan 8 |
Other
Other | 42nd AIAA Aerospace Sciences Meeting and Exhibit |
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Country/Territory | United States |
City | Reno, NV |
Period | 04/1/5 → 04/1/8 |
All Science Journal Classification (ASJC) codes
- Engineering(all)