Control of Flow Separation on Trailing Edge Flap Using a Delta-Shaped Vortex Generators
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/63/3/63_63_83/_pdf
Reference6 articles.
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3. 5) Hummel, D. and Srinivasan, P. S.: Vortex Breakdown Effects on the Low-Speed Aerodynamic Characteristics of Slender Delta Wings in Symmetrical Flow, J. Royal Aeronautics Soc., 71 (1967), pp. 319-322.
4. 7) Rinoie, K., Miyata, K., Kwak, D. Y. and Noguchi, M.: Studies on Vortex Flaps with Rounded Leading-Edges for Supersonic Transport Configuration, J. Aircraft, 41, 4 (2004), pp. 829-838.
5. 8) Kwak, D. Y., Noguchi, M., Shirotake, M. and Rinoie, K.: Rolling Moment Characteristics of Supersonic Transport Configuration at High Incidence Angles, J. Aircraft, 43, 4 (2006), pp. 1112-1119.
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