Design of Vortex Flaps for Reducing Approach Speed of a Supersonic Naval Fighter Aircraft
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-15-5432-2_9
Reference14 articles.
1. E.C. Polhamus, Applying slender wing benefits to military aircraft. J. Aircr. 21(8) (1984). https://doi.org/10.2514/3.45023
2. K.D. Hoffler, D.M. Rao, M.C. Frassinelli, Low-speed aerodynamics of apex fences on a tailless delta configuration. J. Aircr. 25(4) (1988). https://doi.org/10.2514/3.45563
3. D.M. Rao, J.F. Campbell, Vortical flow management techniques. Prog. Sci. 24, (1987). https://doi.org/10.1016/0376-0421(87)90007-8
4. J.M. Luckring, Aerodynamics of strake-wing interactions. J. Aircr. 16(11) (1979). Article No. 78-1202R
5. M.R. Visbal, Computational and physical aspects of vortex breakdown on delta wings. in 33rd AIAA Aerospace Sciences Meeting and Exhibit. Jan (1995). https://doi.org/10.2514/6.1995-585
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