Abstract
The goal of this study is to determine the influence of localized energy addition into supersonic flow on the temperature field and Mach number of the flow, and the shock structure and pressure distribution around a body in the flow. Of particular interest is the possibility of using the flow field perturbations caused by local energy deposition to produce controllable forces and moments on a body in the flow. The design and testing of the experimental facility used in this study is detailed, and comparisons of the performance of the facility are made with CFD calculations.
Original language | English (US) |
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State | Published - 2001 |
Event | 32nd AIAA Plasmadynamics and Lasers Conference 2001 - Anaheim, CA, United States Duration: Jun 11 2001 → Jun 14 2001 |
Other
Other | 32nd AIAA Plasmadynamics and Lasers Conference 2001 |
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Country/Territory | United States |
City | Anaheim, CA |
Period | 6/11/01 → 6/14/01 |
All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering
- Condensed Matter Physics