Visualization measurements of vortex flows
Author:
Affiliation:
1. University of Bristol, Bristol, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46030
Reference23 articles.
1. A theory of the flow past a slender delta wing with leading edge separation
2. Improved calculations of leading-edge separation from slender, thin, delta wings
3. 4Campbell, J. F., Chambers, J. R., and Rumsey, C. L. "Observation of Airplane Flow Fields by Natural Condensation Effects," AIAA Paper 88-0191, Jan.1988.
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