Leading Edge Vortex Flaps on Moderate Sweep Wings- UCAV, Flow Improvement at High Lift AIAA Paper
45th, AIAA aerospace sciences meeting ; 2007 ; Reno, NV
2007-01-01
2007-267-2007-722
Papers in the range 2007 17 to 1467 with gaps. Held on CD-ROM
Aufsatz (Konferenz)
Englisch
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