Effectiveness of vortex generator position and orientation on highly swept wings
Author:
Affiliation:
1. Cranfield Univ., United Kingdom
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2319
Reference5 articles.
1. Corrections for symmetrical swept and tapered wings inrectangular wind tunnels. Acum, W.E.A., R & M2777,April 1950.
2. DERA (Bedford) under agreement 94316100 (1994).
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