An experimental investigation of a fighter aircraft model at high angles of attack
Approved for public release; distribution is unlimited === A low speed wind tunnel investigation was conducted to examine the aerodynamic characteristics of the flowfield around a three percent scale YF-17 lightweight fighter prototype model at high angles of attack using flow visualization and...
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| Format: | Others |
| Language: | en_US |
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Sept
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| Online Access: | http://hdl.handle.net/10945/23224 |