Abstract
In this paper, the application of energy deposition ahead of a blunt cylinder at Mach 3 is investigated. The energy deposition is simulated as a instantaneous high temperature filament in front of the cylinder. A commercial numerical code is used to solve for the Euler equations. The results show a significant momentary decrease in drag coefficient. It is seen that beyond sufficiently long filaments, the magnitude of the drag reduction becomes insensitive to the filament length.
Original language | English (US) |
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DOIs | |
State | Published - 2012 |
Event | 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Nashville, TN, United States Duration: Jan 9 2012 → Jan 12 2012 |
Other
Other | 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
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Country/Territory | United States |
City | Nashville, TN |
Period | 1/9/12 → 1/12/12 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering